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WO2010050714A2 - Apparatus for measuring ground displacement - Google Patents

Apparatus for measuring ground displacement Download PDF

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Publication number
WO2010050714A2
WO2010050714A2 PCT/KR2009/006204 KR2009006204W WO2010050714A2 WO 2010050714 A2 WO2010050714 A2 WO 2010050714A2 KR 2009006204 W KR2009006204 W KR 2009006204W WO 2010050714 A2 WO2010050714 A2 WO 2010050714A2
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WO
WIPO (PCT)
Prior art keywords
sensing means
ground
displacement
dimensional coordinate
sensor
Prior art date
Application number
PCT/KR2009/006204
Other languages
French (fr)
Korean (ko)
Other versions
WO2010050714A3 (en
Inventor
์ด์Šน๋ชฉ
Original Assignee
Lee Seung-Mok
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Lee Seung-Mok filed Critical Lee Seung-Mok
Publication of WO2010050714A2 publication Critical patent/WO2010050714A2/en
Publication of WO2010050714A3 publication Critical patent/WO2010050714A3/en

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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01BMEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B7/00Measuring arrangements characterised by the use of electric or magnetic techniques
    • G01B7/16Measuring arrangements characterised by the use of electric or magnetic techniques for measuring the deformation in a solid, e.g. by resistance strain gauge
    • EFIXED CONSTRUCTIONS
    • E21EARTH OR ROCK DRILLING; MINING
    • E21BEARTH OR ROCK DRILLING; OBTAINING OIL, GAS, WATER, SOLUBLE OR MELTABLE MATERIALS OR A SLURRY OF MINERALS FROM WELLS
    • E21B47/00Survey of boreholes or wells
    • E21B47/02Determining slope or direction
    • E21B47/022Determining slope or direction of the borehole, e.g. using geomagnetism
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01BMEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B21/00Measuring arrangements or details thereof, where the measuring technique is not covered by the other groups of this subclass, unspecified or not relevant
    • G01B21/32Measuring arrangements or details thereof, where the measuring technique is not covered by the other groups of this subclass, unspecified or not relevant for measuring the deformation in a solid
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01BMEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B7/00Measuring arrangements characterised by the use of electric or magnetic techniques

Definitions

  • the present invention relates to a ground displacement measuring apparatus, and more particularly, is inserted into an inclined tube excavated perpendicularly to the ground and moved in the longitudinal direction to detect the ground displacement by contact, but three-dimensional coordinate displacement in accordance with the set measurement timing It relates to a ground displacement measuring device configured to measure in real time.
  • the ground displacement measuring apparatus includes a movable type for measuring a tilting sensor by inserting the sensing means into a tilting tube, and a buried type for inserting and measuring a plurality of sensing means for each measuring depth in the tilting tube.
  • Mobile and buried are optionally used, taking into account their advantages and disadvantages.
  • the mobile type has limitations compared to the buried type in terms of the accuracy of the measurement data, but has the advantage of being able to measure at low cost.
  • FIG. 1 is a configuration diagram showing an example of a conventional ground displacement measuring apparatus.
  • Exemplary ground displacement measuring device is a movable, vertical movement along the inner circumferential surface of the inclined tube 30 excavated underground, the moving unit 20 for detecting the displacement of the ground, and a motor for providing a driving force for vertical movement ( 10) and a measurement unit 5 located on the ground to calculate the ground displacement using the measured value transmitted from the moving unit 20.
  • the moving part 20 is also called a probe.
  • the moving part 20 includes a plurality of wheels 22a and 22b protruding outward, the moving part 20 moves up and down vertically while making a contact state along the inner circumferential surface of the inclined tube 30 when the motor 10 is driven.
  • the moving part 20 moves up and down along the inclined pipe 30, and automatically measures horizontal and vertical inclination degrees when passing through the bent part (symbol A) of the inclined pipe 30 formed by the ground relaxation.
  • Reference numeral F denotes the displacement direction of the ground.
  • the measuring unit 5 calculates and displays the position, direction, and size of the ground displacement by using the horizontal and vertical tilt detection signals received from the moving unit 20, and the operator can use the same to check the ground state in the region. do.
  • a pair of wheels 22a and 22b are provided at the ends of the support part 24, respectively, on the upper side and the lower side, and the support part 24 is installed with a predetermined inclination angle, so the inclination angle from one side to the other side is different.
  • FIG. 2 is a use state diagram showing a measurement example of a conventional ground displacement measuring apparatus.
  • acceleration sensors in the horizontal and vertical directions are installed in the moving unit 20 at 50 cm intervals, for example, to measure inclination at 50 cm intervals. Perform the origin correction at, B1, C1, D1, E1) and measure the ground displacement based on this data.
  • this method is a method of detecting the overall ground displacement by measuring only the inclination of the two axes (x, y), there is a disadvantage that the measurement error and objectivity is inferior.
  • the minimum measuring interval is 50 cm, and the actual inclination measurement is made as follows.
  • the change of the angle is measured while moving the moving part 20 in the order of A1-> B1-> C1-> D1-> E1.
  • the lower wheel 22b at the time of the second measurement comes to the position of the upper wheel 22a at the time of the first measurement, and the second inclination measurement is performed based on the point (reference point). This process is repeated to measure the inclination displacement in the entire inclined tube.
  • the conventional ground displacement measuring apparatus using this method had the following limitations.
  • the present invention has been made in view of the above problems, it is inserted into the inclined tube excavated perpendicular to the ground and moved in its longitudinal direction to detect the ground displacement by contact, but the three-dimensional coordinate displacement in accordance with the set measurement timing It is an object of the present invention to provide a ground displacement measuring device configured to measure in real time.
  • the present invention by using a variety of sensor combinations or by setting a plurality of measurement timings to perform a variety of correction processing for the measurement data, the conventional measurement error caused by mismatch of measurement reference point or puncture verticality, inclination of the inclined pipe It is another object to provide a ground displacement measuring device that solves the problem.
  • the present invention can make the length of the moving portion smaller than the conventional, can accurately measure the sharp and minute inclination having a radius of curvature less than the vertical wheel spacing of the conventional moving portion, and the ground displacement that can be added to the moving portion even in a sharp slope It is another object to provide a measuring device.
  • the ground displacement measuring apparatus of the present invention for achieving the above object is inserted into the inclined tube vertically excavated to the ground is movable in the longitudinal direction, the ground displacement measurement to detect the displacement of the inner surface of the inclined tube by contact type
  • An apparatus comprising: sensing means for measuring a three-dimensional coordinate displacement at every measurement timing when moving in its longitudinal direction in an inclined tube; Timing setting means for setting the measurement timing; Displacement amount calculation means for calculating three-dimensional coordinate displacement data measured by the sensing means as ground displacement; It is configured to include.
  • the sensing means is composed of any one of a three-axis gyro sensor or a three-axis acceleration sensor.
  • the sensing means consists of a combination of either a two-axis gyro sensor or two-axis acceleration sensor and the ground vertical movement distance measuring sensor.
  • the sensing means is composed of a plurality of sensing means having a mutually independent measuring method, and has a function of comparing and correcting the three-dimensional coordinate displacement data measured by each sensing means.
  • the mutual comparison and correction of the three-dimensional coordinate displacement data based on the three-dimensional coordinate displacement data measured by one side sensing means, exceeding a predetermined error range of the three-dimensional coordinate displacement data measured by the other sensing means.
  • the case where the value is indicated is determined to be an error and is processed.
  • the plurality of sensing means includes at least two sensors, and includes a three-axis gyro sensor and a three-axis acceleration sensor.
  • the plurality of sensing means is composed of at least two sensor combinations, the sensor combinations are a combination of a 2-axis gyro sensor and a ground vertical travel distance measurement sensor and a 2-axis acceleration sensor and ground vertical A combination of directional travel distance sensors.
  • the present invention further includes at least one of a ground vertical movement distance measuring sensor and a temperature sensor as auxiliary sensing means, and has a function of correcting three-dimensional coordinate displacement data measured by the sensing means.
  • the timing setting means is provided to set a plurality of mutually independent frequencies as the measurement timing, the function of comparing and correcting the three-dimensional coordinate displacement data measured by the sensing means for each frequency It is provided.
  • the sensing means is composed of a plurality of sensing means
  • the timing setting means is provided to set a plurality of frequencies independent of each sensing means for each of the sensing means, each of the sensing means And a function of comparing and correcting the measured three-dimensional coordinate displacement data with each other.
  • the mutual comparison and correction of the three-dimensional coordinate displacement data is based on the three-dimensional coordinate displacement data measured by setting one frequency as the measurement timing, and the three-dimensional measured by setting another frequency as the measurement timing. It is configured to determine and process a case in which a value exceeding a preset error range among coordinate displacement data is regarded as an error.
  • the moving unit measures the displacement in the three-dimensional (or three-axis) direction in real time according to the measurement timing during the movement in the inclined tube, the measurement process is not necessary without considering the minimum measurement interval or reference point. This solves the conventional measurement error problem caused by the mismatch of the reference point or the perforated vertical degree, the inclination of the inclined tube.
  • the length of the moving part can be made smaller than in the related art, a sharp and minute inclination having a radius of curvature of the upper and lower wheel intervals of the moving part can be accurately measured, and there is an advantage that the moving part can be inserted even in a sharp inclination.
  • FIG. 1 is a configuration diagram showing an example of a conventional ground displacement measuring apparatus
  • FIG. 2 is a use state diagram showing a measurement example of a conventional ground displacement measuring apparatus
  • FIG. 3 and 4 is a block diagram of a ground displacement measuring apparatus according to an embodiment of the present invention.
  • FIG. 6 is an operation flow chart of the ground displacement measuring apparatus according to an embodiment of the present invention.
  • FIG. 8 is a block diagram of a ground displacement measuring apparatus according to another embodiment of the present invention.
  • FIG. 10 is a block diagram of a ground displacement measuring apparatus according to another embodiment of the present invention.
  • FIG. 11 is an operation flow chart of the ground displacement measuring apparatus according to another embodiment of the present invention.
  • FIG. 12 is a block diagram of a ground displacement measuring apparatus according to another embodiment of the present invention.
  • FIG. 13 is an operation flow chart of the ground displacement measuring apparatus according to another embodiment of the present invention.
  • FIG 3 and 4 is a configuration diagram of a ground displacement measuring apparatus according to an embodiment of the present invention
  • Figure 5 is a state diagram of the ground displacement measuring apparatus according to an embodiment of the present invention
  • Figure 6 is an embodiment of the present invention This is an example of the operation flow chart of the ground displacement measuring device.
  • Ground displacement measuring apparatus of the present embodiment is a movable, vertical movement along the inner circumferential surface of the inclined pipe 500 excavated underground, the moving unit 400 for detecting the displacement of the ground, and located on the ground wire (or signal line, 300 It is configured to include a calculation control unit 200 connected to the through and to calculate the ground displacement using the measured value transmitted from the moving unit 400.
  • the moving part 400 is also called a probe, and moves vertically by a motor 410 or a known driving means that performs an equivalent function.
  • Such drive means include both automatic and manual methods.
  • the moving part 400 includes a plurality of wheels 410a and 410b protruding outward, the moving part 400 is vertically moved up and down while making a contact state along the inner circumferential surface of the inclined tube 500 when the motor 410 is driven.
  • Such a structure may be viewed as a structure similar to the conventional ground displacement measuring apparatus described with reference to FIGS. 1 and 2. That is, the ground displacement measuring apparatus of the present embodiment is inserted into the inclined tube 500 excavated perpendicularly to the ground and is movable in the longitudinal direction (z direction), and only if the displacement of the inner surface of the inclined tube is detected by a contact type.
  • the structure of the wheels 410a, 410b), the shape of the moving unit 400, etc. are not particularly limited to any one configuration.
  • the moving part 400 is provided with a sensor part 100 provided with the sensing means 110, the sensing means 110 is the timing setting means 210 when the moving part 400 moves in the longitudinal direction in the inclined tube. Each 3D coordinate displacement is measured in real time.
  • an inertial sensor such as a three-axis gyro sensor or a three-axis acceleration sensor, which is preferably implemented by MEMS (Micro Electro Mechanical System) technology, is used.
  • MEMS Micro Electro Mechanical System
  • accelerometers have a volume of about ((2-3) mm) 3 or less and their accuracy is increasing every year.
  • MEMS gyro sensor of the present embodiment for example, a known vibration type gyro sensor using the force of Coriolis can be applied.
  • MEMS acceleration sensor for example, a known capacitive acceleration sensor composed of a mass body and a banet or the like, or An acceleration sensor using a piezo resistance change may be applied.
  • Gyro sensors or acceleration sensors are all sensors that use inertial force to detect movement.
  • the gyro sensor or acceleration sensor measures the inertial force acting on the mass provided in the sensor based on the electromagnetic principle and obtains the angular velocity or acceleration value. Integrating the angular velocity or acceleration value in this way into consideration of the equations of motion results in obtaining the coordinate displacement during the movement. For example, the coordinate displacement value is obtained by integrating the acceleration value twice.
  • the sensing means 110 measures the three-dimensional coordinate displacement in real time for each measurement timing set by the timing setting means 210. Will be measured.
  • the sensing means 110 may be a structure in which three single-axis acceleration sensors are installed by combining the three-axis acceleration sensors at 90-degree intervals in the x, y, and z directions, respectively, and the two-axis acceleration sensor and the single-axis acceleration sensor. It may be a combination structure of, or may be a single packaged three-axis acceleration sensor. That is, as long as the angular velocity or acceleration of the three axes can be measured, the structure of the sensing means 110 is not particularly limited to any one configuration.
  • an amplifier circuit and an AD converter which are commonly used in measuring signal processing may be provided in the sensor unit 100, but are not separately illustrated in the drawings.
  • the amplifying circuit and the AD converter may be installed in the sensor unit 100 as each unit, or may be provided in an integrated form in a gyro sensor or an acceleration sensor module according to the recent sensor module trend.
  • the three-dimensional coordinate displacement data measured by the sensing means 110 is transmitted to the calculation control unit 200 located on the ground through the wire (or signal line, 300), displacement calculation unit 220 provided in the calculation control unit 200 It is calculated by ground displacement and displayed to the operator. Through this, the worker can grasp the position, direction, and size of the ground relaxation or its displacement. This entire process can be understood in more detail through the operation flow chart consisting of the steps S520 to S560 of FIG.
  • the process of measuring the three-dimensional coordinate displacement by the gyro sensor or the acceleration sensor can be understood as follows.
  • the gyro sensor or the acceleration sensor is measured at the immediately preceding measurement point at each set frequency point.
  • the relative position of the moving unit at the current measurement time is measured based on the position of the moving unit.
  • the moving speed of the moving unit 400 is preferably a fixed speed, but there is no problem even if the speed changes during the movement.
  • the three-dimensional coordinate displacement calculation may be performed directly in the sensor unit 100, or may be performed in the ground operation control unit 200.
  • the sensor unit 100 installed in the moving unit 400 may be manufactured in the form of a system on chip (SoC), and the three-dimensional coordinate displacement module may be manufactured in the form of a single chip in the system on chip (SoC).
  • SoC system on chip
  • the gyro sensor (or the acceleration sensor), the amplification circuit, and the AD converter are installed in the sensor unit 100, and the three-dimensional coordinate displacement calculation may be configured to be performed by the ground operation control unit 200.
  • the operation control unit 200 is provided with a power supply 230 and a display unit (not shown), and may be additionally provided with additional functional elements included in a conventional measuring device.
  • timing setting unit 210 is illustrated as being installed in the operation control unit 200, it may be installed in the sensor unit 100 as necessary.
  • the measurement timing set through the timing setting means 210 means a measurement time interval in which the sensing means 110 performs a sensing operation, and can be understood as a frequency concept.
  • the sensing means 110 performs 25 sensing operations per second, and the sensing operation is performed during the movement of the moving unit 400. This means that 25 coordinate displacement measurements are made per second.
  • the ground displacement measuring apparatus Since the coordinate displacement measurement is performed in such a manner, the ground displacement measuring apparatus according to the present invention does not have to consider a minimum measurement interval or a reference point, unlike the conventional method, and the measurement process is continuously performed in real time. This solves the problem of conventional measurement errors caused by torsional torsion.
  • the moving part 400 since the length of the moving part 400 can be made smaller than the conventional method using a small sensor implemented by MEMS technology, the moving part 400 has a radius of curvature of less than or equal to the interval between the upper and lower wheels 410a and 410b.
  • the fine inclination can be measured precisely, and it provides the advantage that the moving part can be inserted even in the steep inclination.
  • the present embodiment illustrates a three-axis gyro sensor or three-axis acceleration sensor implemented by MEMS technology, but if the sensing means that can perform the sensing operation for the three-dimensional coordinate displacement in accordance with the measurement timing during the movement of the moving part
  • the present invention is not limited to the illustrated ones, but is included in the scope of the present invention. In particular, it can be preferably applied if it has a small size.
  • FIG 7 is an operation flowchart of the ground displacement measuring apparatus according to another embodiment of the present invention.
  • the sensing means comprises a combination of either a two-axis gyro sensor or a two-axis acceleration sensor and a ground vertical movement distance measuring sensor.
  • a three-axis gyroscope or a three-axis acceleration sensor is used to measure the three-dimensional coordinate displacement, but in this embodiment, a two-axis gyroscope or two-axis acceleration sensing in the x- and y-axis directions
  • the three-dimensional coordinate displacement is measured by combining the sensor and the vertical distance (z direction) moving distance measuring sensor.
  • the z axis is a direction in which the moving part 400 moves along the inclined tube, so that the ground vertical direction (z direction) movement that directly measures the moving amount is considered when a physical obstacle occurs in the moving path.
  • Using a distance sensor may be better in terms of measurement reliability than a method of calculating displacement by measuring an inertia physical quantity such as acceleration.
  • Ground vertical direction (z direction) movement distance measuring sensor may be a known sensing means for measuring the movement amount of the moving unit 400 through the transfer amount of the wire 300, for example, the ground vertical in the following manner Measure the direction.
  • the measuring wheels when the measuring wheels are fixed to one point of the ground in contact with the wire 300 connected to the moving unit 400, the measuring wheels move with the wire 300 when the wire 300 is moved. It is rotated by the contact force.
  • the absolute value of the moving distance in the z-direction of the moving part 400 connected to the wire 300 is relatively simple. It can be measured.
  • the measuring wheel may be used in combination with the support roller 420 of the wire 300 shown in FIG. 5, and may be installed at any position in contact with the wire 300.
  • any sensing method capable of measuring the moving distance of the wire 300 regardless of whether it is contact or non-contact may be used in any known manner.
  • the conventional ground displacement measuring apparatus illustrated in FIGS. 1 and 2 repeats the stand-by-going measurement intervals, so that an error in the z direction is inevitably generated, and thus, a process of recognizing and controlling the moving distance in the z direction may be complicated. There was only. However, since the ground displacement measuring apparatus according to the present embodiment is a method of raising and lowering the moving unit 400 at a constant speed, the position and moving distance in the z direction can be accurately measured even through a simple algorithm.
  • FIG 8 is a block diagram of a ground displacement measuring apparatus according to another embodiment of the present invention
  • Figure 9 is a flow chart of the ground displacement measuring apparatus according to another embodiment of the present invention.
  • the sensing means of this embodiment is composed of a plurality of sensing means (112, 114) having a mutually independent measurement method.
  • both gyro and acceleration sensors use inertial forces to detect movement.
  • the gyro sensor detects the angular velocity using the Coriolis force acting on the mass that rotates
  • the acceleration sensor measures the force acting on the mass of linear movement and uses the equation of motion to measure the acceleration. It is a way of detection.
  • the displacement amount calculating means 220 performs a function of comparing and correcting the three-dimensional coordinate displacement data measured by the sensing means.
  • the sensing means 112 and 114 can measure the coordinate displacement of three axes as in the previous embodiment, and the structure of the sensing means is not particularly limited to any one configuration. In addition, it is not necessarily limited to two, it is natural that two or more may be provided as long as different physical measurement principles are used.
  • FIG. 10 is a block diagram of a ground displacement measuring apparatus according to another embodiment of the present invention
  • Figure 11 is a flow chart of the ground displacement measuring apparatus according to another embodiment of the present invention.
  • the moving unit 400 along with the sensing means 110 for measuring in real time the three-dimensional coordinate displacement for each measurement timing set by the timing setting means 210 when moving in the longitudinal direction in the inclined tube,
  • the sensing means 150 is further provided.
  • the auxiliary sensing means 150 provides a function of correcting the three-dimensional coordinate displacement data measured by the sensing means 110, one of the ground vertical direction (z direction) moving distance measuring sensor 154 or the temperature sensor 156 Or combinations thereof.
  • the auxiliary sensing means 150 is a ground vertical direction (z direction) moving distance measuring sensor ( 154 or one or a combination of temperature sensors 156.
  • the auxiliary sensing means 150 includes both the ground vertical direction (z direction) moving distance measuring sensor 154 and the temperature sensor 156 to increase the accuracy of the measured value.
  • the sensing means 110 is made of a combination of any one of the two-axis gyro sensor or two-axis acceleration sensor and the ground vertical movement distance measuring sensor, only the temperature sensor 156 to the secondary sensing means ( 150).
  • auxiliary sensing means 150 for correcting the measurement values in various ways.
  • the temperature sensor 156 serves to correct a measurement error of the gyro sensor or the acceleration sensor that may be generated by the external temperature environment during the measurement process.
  • the gyro sensor or the acceleration sensor used in this embodiment is formed of a multilayer thin film structure using, for example, a silicon wafer or various electrodes or dielectric thin films.
  • Residual stresses in the thin film structure include residual stresses caused by differences in basic crystal grains such as crystal defects or crystal constants, and thermal residual stresses generated because the coefficient of thermal expansion differs for each material during temperature rise.
  • the thermal residual stress generated when the temperature rises may represent a very large value (hundreds of GPa order) according to the temperature, the error value according to the temperature change of the gyro sensor or the acceleration sensor is dataged and the temperature sensor 156 is used. When the error is corrected using the measured temperature value, the accuracy of the measured value can be further increased.
  • FIG. 12 is a block diagram of a ground displacement measuring apparatus according to another embodiment of the present invention
  • Figure 13 is a flow chart of the ground displacement measuring apparatus according to another embodiment of the present invention.
  • the timing setting means 210 is provided to set a plurality of independent frequencies as the measurement timing, set different frequency values as the measurement timings for each of the plurality of movement measuring processes, and sense each sensing measurement process. And means for comparing and correcting the three-dimensional coordinate displacement data measured by the means 112,114.
  • the measurement is performed while moving the moving unit 400 a plurality of times, and the measurement is performed by setting the measurement timing of the sensing means 112 and 114 to 25 Hz during the first movement measurement, and the sensing means 112 and 114 during the second movement measurement.
  • the measurement timing is set to 100 Hz, and the three-dimensional coordinate displacements of the first measurement and the second measurement are compared and corrected.
  • 25 measurements per second can be obtained with a large radius of curvature and 100 seconds per second with a small radius of curvature. More accurate values can be obtained when using a frequency that is high enough to measure twice.
  • the reliability of the data may be adjusted to improve the reliability of the entire data. For example, if a small curvature radius gives high reliability to high frequency data, and vice versa, high reliability to low frequency data and reflects this reliability in the displacement operation, a more accurate calculation It becomes possible.
  • a and B data obtained at high frequency and low frequency are A and B, respectively.
  • the average value a can be obtained as follows.
  • Equation 1 n is the total number of data, โ‡ A , โ‡ B represents the reliability coefficient of the A, B value, respectively, which is determined to reflect the radius of curvature.
  • the A and B values are the coordinate displacement values of the specific points measured at different frequencies, but the two measurement values where the measurement points are actually matched according to the frequency setting state can be directly compared.
  • Ground displacement values obtained in discrete data form for each frequency over a range may be obtained in the form of continuous data through interpolation, and then compared for each predetermined point set by an operator.
  • the measurement may be performed a plurality of times by varying the frequency, and the error may be reduced and the accuracy may be increased by correcting the measured value in the above manner.
  • the frequency that can be set as the measurement timing is preferably in the range of 1-100 Hz, and can be electronically controlled by the timing setting means 210.
  • the mutual comparison and correction of the three-dimensional coordinate displacement data is based on the three-dimensional coordinate displacement data measured by setting one frequency as the measurement timing, and among the three-dimensional coordinate displacement data measured by setting another frequency as the measurement timing. This is done through the process of judging the case where the value is over the set error range as an error. This entire process can be understood in more detail through the operation flow chart consisting of the steps S1010 to S1080 of FIG.
  • At least one of the ground vertical movement distance measuring sensor 154 or the temperature sensor 156 is further provided as the auxiliary sensing means 150, the three-dimensional measured by the sensing means (112, 114) By providing the function of correcting the coordinate displacement data, the effect of further increasing the measurement accuracy can be obtained.
  • the sensing means is composed of a plurality of sensing means (112, 114), the timing setting means 210 is provided to set a plurality of frequencies independent of each sensing means for each of the sensing means, each sensing means (112,114) ) Compares and corrects the three-dimensional coordinate displacement data measured by
  • the measurement timing of the first sensing means 112 is set to 25 Hz
  • the measurement timing of the second sensing means 114 is set to 100 Hz to perform the measurement
  • the three-dimensional coordinate displacement measured by the first sensing means 112 and the three-dimensional coordinate displacement measured by the second sensing means 114 are compared and corrected.
  • the first sensing means 112 and the second sensing means 114 do not necessarily use the same type of sensor, but may use other types of sensors.
  • the mutual comparison and correction of the three-dimensional coordinate displacement data is based on the three-dimensional coordinate displacement data measured by setting one frequency as the measurement timing, and among the three-dimensional coordinate displacement data measured by setting another frequency as the measurement timing.
  • the case in which a value exceeding a preset error range is determined as an error is made through a process of processing. This entire process can be understood in more detail through the operation flow chart consisting of the steps S1210 to S1280 of FIG.
  • At least one of the ground vertical movement distance measuring sensor 154 or the temperature sensor 156 is further provided as the auxiliary sensing means 150, the three-dimensional measured by the sensing means (112, 114) By providing the function of correcting the coordinate displacement data, the effect of further increasing the measurement accuracy can be obtained.

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Abstract

The present invention relates to an apparatus for measuring ground displacement, and specifically to an apparatus for measuring ground displacement that is inserted into an inclined tube that is drilled perpendicularly into the ground to enable movement along the length direction thereof and sensing by contact of the displacement inside the inclined tube, comprising: a sensing means that measures 3-dimensional coordinate displacement at each measurement timing when moving lengthwise in the inclined tube; a timing setup means that sets up said measurement timing; and a displacement calculation means that calculates the ground displacement from the 3-dimensional coordinate displacement data measured at said sensing means; because the moving part measures the displacement in a 3-dimensional (or 3-axial) direction on a real time basis according to the measurement timing while the moving part is moving within the inclined tube, the measurement process takes place without the need to take into account the minimum measurement interval, reference point, etc., thus, the problems of the prior art regarding measurement error due to inconsistency of the reference point, perpendicularity of punching, twist of the inclined tube, etc., are resolved.

Description

์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜Ground displacement measuring device
๋ณธ ๋ฐœ๋ช…์€ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜์— ๊ด€ํ•œ ๊ฒƒ์œผ๋กœ์„œ, ๋ณด๋‹ค ์ƒ์„ธํ•˜๊ฒŒ๋Š” ์ง€๋ฐ˜์— ์ˆ˜์ง์œผ๋กœ ๊ตด์ฐฉ๋œ ๊ฒฝ์‚ฌ๊ด€์— ์‚ฝ์ž…๋˜์–ด ๊ทธ ๊ธธ์ด๋ฐฉํ–ฅ์œผ๋กœ ์ด๋™ํ•˜๋ฉด์„œ ์ ‘์ด‰์‹์œผ๋กœ ์ง€๋ฐ˜ ๋ณ€์œ„๋ฅผ ๊ฐ์ง€ํ•˜๋˜, ์„ค์ •๋œ ์ธก์ • ํƒ€์ด๋ฐ์— ๋งž์ถฐ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„๋ฅผ ์‹ค์‹œ๊ฐ„์œผ๋กœ ์ธก์ •ํ•˜๋„๋ก ๊ตฌ์„ฑ๋œ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜์— ๊ด€ํ•œ ๊ฒƒ์ด๋‹ค. The present invention relates to a ground displacement measuring apparatus, and more particularly, is inserted into an inclined tube excavated perpendicularly to the ground and moved in the longitudinal direction to detect the ground displacement by contact, but three-dimensional coordinate displacement in accordance with the set measurement timing It relates to a ground displacement measuring device configured to measure in real time.
์ง€ํ•˜์‹œ์„ค๋ฌผ์˜ ์‹œ๊ณต์„ ์œ„ํ•ด์„œ๋Š” ๊ตด์ฐฉ์ด๋‚˜ ์„ฑํ†  ์‹œ์— ๊ณต๋™ ํ˜„์ƒ ๋ฐ ์ง€ํ•˜์ˆ˜์œ„์˜ ๋ณ€์œ„๋Ÿ‰ ๋“ฑ ์ฃผ๋ณ€ ์˜ํ–ฅ์œผ๋กœ ์ธํ•œ ์ง€๋ฐ˜์˜ ๋ณ€์œ„(ํ† ๋ฆฝ์ž์˜ ์ˆ˜ํ‰๊ฒฝ์‚ฌ๋Ÿ‰์˜ ์œ„์น˜์™€ ๋ฐฉํ–ฅ, ํฌ๊ธฐ ๋“ฑ)๋ฅผ ์ธก์ •ํ•˜๋Š” ํ•˜๋Š” ๊ฒƒ์ด ํ•„์ˆ˜์ ์ด๋‹ค. For the construction of underground facilities, it is essential to measure the displacement of the ground (location, direction, size, etc. of the horizontal slope of the soil) due to peripheral influences such as cavitation and groundwater displacement during excavation or filling.
์˜ˆ๋ฅผ ๋“ค์–ด, ์ง€ํ•˜์ฒ  ๋ฐ ํ™๋ง‰์ด ๊ณต์‚ฌ์˜ ๊ตด์ฐฉ๊ณต์‚ฌ ๋“ฑ์— ์žˆ์–ด์„œ, ํ† ๋ฅ˜๋ฒฝ ๊ฐ•์„ฑ์ด๋‚˜ ํ† ์งˆ์— ๋”ฐ๋ผ ์ •๋„์˜ ์ฐจ์ด๋Š” ์žˆ์ง€๋งŒ ์ผ๋ฐ˜์ ์œผ๋กœ ๊ตดํ† ๋œ ๋ฐฉํ–ฅ์œผ๋กœ ํšก๋ฐฉํ–ฅ ๋ณ€์œ„๊ฐ€ ๋ฐœ์ƒํ•˜๊ณ , ์ด์— ๋”ฐ๋ฅธ ์ง€๋ฐ˜์นจํ•˜ํ˜„์ƒ์ด ์œ ๋ฐœ๋˜์–ด ์ธ์ ‘ํ•œ ์ฃผ์š”๊ตฌ์กฐ๋ฌผ ๋“ฑ์— ์‹ฌ๊ฐํ•œ ํ”ผํ•ด๋ฅผ ๋ฐœ์ƒ์‹œํ‚ฌ ์ˆ˜ ์žˆ๋‹ค. ์ด๋กœ ์ธํ•ด ์‹œ๊ณต์ž๋Š” ํ•ด๋‹น ์ง€์—ญ ๋‚ด์— ๊ฒฝ์‚ฌ๊ด€์„ ๊ตด์ฐฉํ•˜๊ณ , ์‹œ๊ณต๊ณผ์ • ๋ฐ ์ผ์ •๊ธฐ๊ฐ„์ด ์ง€๋‚œ ํ›„์— ์ง€๋ฐ˜์ด์™„์— ๋”ฐ๋ฅธ ๊ฒฝ์‚ฌ๊ด€ ๋‚ด์˜ ๋ณ€์œ„๋Ÿ‰์„ ์ธก์ •ํ•˜์—ฌ ์•ˆ์ „๋„๋ฅผ ์˜ˆ์ธกํ•˜๊ฒŒ ๋œ๋‹ค. For example, in the excavation work of subway and earthquake works, there is a difference in degree depending on the earth wall stiffness and soil quality, but in general, transverse displacement occurs in the excavated direction, and ground subsidence is caused, resulting in adjacent main structures. It can cause serious damage. For this reason, the contractor excavates the inclined tube in the area, and after the construction process and a certain period of time, by measuring the displacement amount in the inclined tube according to the ground relaxation to predict the safety.
์ด๋Ÿฌํ•œ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜์—๋Š” ๊ฒฝ์‚ฌ๊ฐ์ง€๋ฅผ ์œ„ํ•œ ์„ผ์‹ฑ์ˆ˜๋‹จ์„ ๊ฒฝ์‚ฌ๊ด€ ๋‚ด์— ์‚ฝ์ž…ํ•˜์—ฌ ์ด๋™์‹์œผ๋กœ ๊ณ„์ธกํ•˜๋Š” ์ด๋™์‹๊ณผ, ๋‹ค์ˆ˜๊ฐœ์˜ ์„ผ์‹ฑ์ˆ˜๋‹จ์„ ๊ฒฝ์‚ฌ๊ด€ ๋‚ด์— ์ธก์ • ๊นŠ์ด๋ณ„๋กœ ์‚ฝ์ž… ์„ค์น˜ํ•˜์—ฌ ๊ณ„์ธกํ•˜๋Š” ๋งค์„ค์‹์ด ์žˆ๋‹ค. The ground displacement measuring apparatus includes a movable type for measuring a tilting sensor by inserting the sensing means into a tilting tube, and a buried type for inserting and measuring a plurality of sensing means for each measuring depth in the tilting tube.
์ด๋™์‹๊ณผ ๋งค์„ค์‹์€ ๊ฐ๊ฐ์˜ ์žฅ๋‹จ์ ์„ ๊ณ ๋ คํ•˜์—ฌ ์„ ํƒ์ ์œผ๋กœ ์‚ฌ์šฉ๋œ๋‹ค. ์˜ˆ๋ฅผ ๋“ค์–ด, ์ด๋™์‹์€ ์ธก์ • ๋ฐ์ดํ„ฐ์˜ ์ •ํ™•์„ฑ ๋ฉด์—์„œ ๋งค์„ค์‹์— ๋น„ํ•ด ํ•œ๊ณ„๊ฐ€ ์žˆ๊ธฐ๋Š” ํ•˜์ง€๋งŒ, ์ €๋ ดํ•œ ๋น„์šฉ์œผ๋กœ ์ธก์ •์ด ๊ฐ€๋Šฅํ•˜๋‹ค๋Š” ์žฅ์ ์„ ๊ฐ–๊ณ  ์žˆ๋‹ค. Mobile and buried are optionally used, taking into account their advantages and disadvantages. For example, the mobile type has limitations compared to the buried type in terms of the accuracy of the measurement data, but has the advantage of being able to measure at low cost.
๋„ 1์€ ์ข…๋ž˜์˜ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜์˜ ์ผ์˜ˆ๋ฅผ ๋‚˜ํƒ€๋‚ธ ๊ตฌ์„ฑ๋„์ด๋‹ค. 1 is a configuration diagram showing an example of a conventional ground displacement measuring apparatus.
์˜ˆ์‹œ๋œ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜๋Š” ์ด๋™์‹์œผ๋กœ์„œ, ์ง€ํ•˜์— ๊ตด์ฐฉ๋œ ๊ฒฝ์‚ฌ๊ด€(30)์˜ ๋‚ด์ฃผ๋ฉด์„ ๋”ฐ๋ผ ์ˆ˜์ง ์ด๋™๋˜์–ด ์ง€๋ฐ˜์˜ ๋ณ€์œ„๋ฅผ ๊ฐ์ง€ํ•˜๋Š” ์ด๋™๋ถ€(20)์™€, ์ˆ˜์ง๋ฐฉํ–ฅ ์ด๋™์„ ์œ„ํ•œ ๊ตฌ๋™๋ ฅ์„ ์ œ๊ณตํ•˜๋Š” ๋ชจํ„ฐ(10), ์ง€์ƒ์— ์œ„์น˜ํ•˜์—ฌ ์ด๋™๋ถ€(20)์—์„œ ์ „์†กํ•œ ์ธก์ •๊ฐ’์„ ์ด์šฉํ•˜์—ฌ ์ง€๋ฐ˜ ๋ณ€์œ„๋ฅผ ์—ฐ์‚ฐํ•˜๋Š” ๊ณ„์ธก๋ถ€(5)๋ฅผ ํฌํ•จํ•˜์—ฌ ๊ตฌ์„ฑ๋œ๋‹ค. ์ด๋™๋ถ€(20)๋Š” ํ”„๋กœ๋ธŒ(probe)๋ผ๊ณ ๋„ ํ•œ๋‹ค. Exemplary ground displacement measuring device is a movable, vertical movement along the inner circumferential surface of the inclined tube 30 excavated underground, the moving unit 20 for detecting the displacement of the ground, and a motor for providing a driving force for vertical movement ( 10) and a measurement unit 5 located on the ground to calculate the ground displacement using the measured value transmitted from the moving unit 20. The moving part 20 is also called a probe.
์ด๋™๋ถ€(20)๋Š” ์™ธ์ธก์œผ๋กœ ๋Œ์ถœ๋œ ๋ณต์ˆ˜์˜ ๋ฐ”ํ€ด(22a,22b)๋ฅผ ๊ตฌ๋น„ํ•˜๋ฏ€๋กœ, ๋ชจํ„ฐ(10)์˜ ๊ตฌ๋™์‹œ ๊ฒฝ์‚ฌ๊ด€(30)์˜ ๋‚ด์ฃผ๋ฉด์„ ๋”ฐ๋ผ ์ ‘์ด‰ ์ƒํƒœ๋ฅผ ๋งŒ๋“ค๋ฉด์„œ ์ˆ˜์ง์œผ๋กœ ์Šนํ•˜๊ฐ•๋œ๋‹ค. Since the moving part 20 includes a plurality of wheels 22a and 22b protruding outward, the moving part 20 moves up and down vertically while making a contact state along the inner circumferential surface of the inclined tube 30 when the motor 10 is driven.
์ด๋™๋ถ€(20)๋Š” ๊ฒฝ์‚ฌ๊ด€(30)์„ ๋”ฐ๋ผ ์Šนํ•˜๊ฐ• ํ•˜๋Š”๋ฐ, ์ง€๋ฐ˜์ด์™„์— ์˜ํ•ด ํ˜•์„ฑ๋œ ๊ฒฝ์‚ฌ๊ด€(30)์˜ ๊ตด๊ณก๋ถ€(๋„๋ฉด๋ถ€ํ˜ธ A)๋ฅผ ํ†ต๊ณผํ•  ๋•Œ ์ˆ˜ํ‰ ๋ฐ ์ˆ˜์ง๊ฒฝ์‚ฌ๋„๋ฅผ ์ž๋™ ์ธก์ •ํ•˜์—ฌ ์ด๋ฅผ ์ง€์ƒ์˜ ๊ณ„์ธก๋ถ€(5)์— ์ „์†กํ•œ๋‹ค. ๋„๋ฉด๋ถ€ํ˜ธ F๋Š” ์ง€๋ฐ˜์˜ ๋ณ€์œ„ ๋ฐฉํ–ฅ์„ ๋‚˜ํƒ€๋‚ธ๋‹ค.The moving part 20 moves up and down along the inclined pipe 30, and automatically measures horizontal and vertical inclination degrees when passing through the bent part (symbol A) of the inclined pipe 30 formed by the ground relaxation. Send to (5). Reference numeral F denotes the displacement direction of the ground.
๊ณ„์ธก๋ถ€(5)๋Š” ์ด๋™๋ถ€(20)๋กœ๋ถ€ํ„ฐ ์ˆ˜์‹ ๋œ ์ˆ˜ํ‰ ๋ฐ ์ˆ˜์ง๊ฒฝ์‚ฌ ๊ฐ์ง€์‹ ํ˜ธ๋ฅผ ์ด์šฉํ•˜์—ฌ ์ง€๋ฐ˜๋ณ€์œ„์˜ ์œ„์น˜์™€ ๋ฐฉํ–ฅ, ํฌ๊ธฐ๋ฅผ ์—ฐ์‚ฐํ•˜์—ฌ ๋””์Šคํ”Œ๋ ˆ์ดํ•˜๊ณ , ์ž‘์—…์ž๋Š” ์ด๋ฅผ ์ด์šฉํ•˜์—ฌ ํ•ด๋‹น ์ง€์—ญ ๋‚ด์˜ ์ง€๋ฐ˜์ƒํƒœ๋ฅผ ํ™•์ธํ•  ์ˆ˜ ์žˆ๊ฒŒ ๋œ๋‹ค. The measuring unit 5 calculates and displays the position, direction, and size of the ground displacement by using the horizontal and vertical tilt detection signals received from the moving unit 20, and the operator can use the same to check the ground state in the region. do.
์˜ˆ์‹œ๋œ ์ด๋™๋ถ€(20)์—๋Š” ์ƒ์ธก๊ณผ ํ•˜์ธก์— ๊ฐ๊ฐ ํ•œ์Œ์˜ ๋ฐ”ํ€ด(22a,22b)๊ฐ€ ์ง€์ง€๋ถ€(24)์˜ ๋๋‹จ์— ๊ฐ๊ฐ ๊ตฌ๋น„๋˜์–ด ์žˆ์œผ๋ฉฐ, ์ง€์ง€๋ถ€(24)๊ฐ€ ์ผ์ • ๊ฒฝ์‚ฌ๊ฐ์„ ๊ฐ–๊ณ  ์„ค์น˜๋˜๋ฏ€๋กœ ์ผ์ธก์—์„œ ํƒ€์ธก์œผ๋กœ ๊ฒฝ์‚ฌ๊ฐ์„ ๊ฐ–๊ณ  ์„ค์น˜๋œ๋‹ค. In the illustrated moving part 20, a pair of wheels 22a and 22b are provided at the ends of the support part 24, respectively, on the upper side and the lower side, and the support part 24 is installed with a predetermined inclination angle, so the inclination angle from one side to the other side is different. Installed with
๋„ 2๋Š” ์ข…๋ž˜์˜ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜์˜ ์ธก์ •์˜ˆ๋ฅผ ๋‚˜ํƒ€๋‚ธ ์‚ฌ์šฉ์ƒํƒœ๋„์ด๋‹ค. 2 is a use state diagram showing a measurement example of a conventional ground displacement measuring apparatus.
๋„ 1์— ์˜ˆ์‹œ๋œ ์ข…๋ž˜์˜ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜์—๋Š” ์ˆ˜ํ‰ ๋ฐ ์ˆ˜์ง ๋ฐฉํ–ฅ์˜ ๊ฐ€์†๋„ ์„ผ์„œ๊ฐ€ ์˜ˆ๋ฅผ ๋“ค์–ด, 50cm ๊ฐ„๊ฒฉ์œผ๋กœ ์ด๋™๋ถ€(20) ๋‚ด์— ์„ค์น˜๋˜์–ด 50cm ๊ฐ„๊ฒฉ์œผ๋กœ ๊ฒฝ์‚ฌ๋„๋ฅผ ์ธก์ •ํ•˜๊ฒŒ ๋˜๋Š”๋ฐ, ๊ฐ๊ฐ์˜ ์ธก์ • ์ง€์ (A1,B1,C1,D1,E1)์—์„œ ์›์  ๋ณด์ • ๋“ฑ์„ ์‹ค์‹œํ•˜๊ณ  ์ด ๋ฐ์ดํ„ฐ๋ฅผ ๊ธฐ๋ฐ˜์œผ๋กœ ์ง€๋ฐ˜๋ณ€์œ„๋Ÿ‰์„ ์ธก์ •ํ•œ๋‹ค.In the conventional ground displacement measuring apparatus illustrated in FIG. 1, acceleration sensors in the horizontal and vertical directions are installed in the moving unit 20 at 50 cm intervals, for example, to measure inclination at 50 cm intervals. Perform the origin correction at, B1, C1, D1, E1) and measure the ground displacement based on this data.
๊ทธ๋Ÿฌ๋‚˜, ์ด๋Ÿฌํ•œ ๋ฐฉ์‹์€ 2์ถ•(x,y)์˜ ๊ฒฝ์‚ฌ๋„๋งŒ ์ธก์ •ํ•˜์—ฌ ์ „์ฒด์ ์ธ ์ง€๋ฐ˜ ๋ณ€์œ„๋ฅผ ํƒ์ง€ํ•˜๋Š” ๋ฐฉ์‹์œผ๋กœ์„œ, ์ธก์ •์˜ ์˜ค์ฐจ์™€ ๊ฐ๊ด€์„ฑ์ด ๋–จ์–ด์ง„๋‹ค๋Š” ๋‹จ์ ์ด ์žˆ๋‹ค. However, this method is a method of detecting the overall ground displacement by measuring only the inclination of the two axes (x, y), there is a disadvantage that the measurement error and objectivity is inferior.
์ด๋™๋ถ€(20)์—์„œ ์ƒํ•˜ ๋ฐ”ํ€ด(22a,22b)๊ฐ„ ๊ฑฐ๋ฆฌ๊ฐ€ ์˜ˆ๋ฅผ ๋“ค์–ด 50cm ์ด๋ฉด ์ตœ์†Œ ์ธก์ •๊ฐ„๊ฒฉ์ด 50cm ๊ฐ€ ๋˜๋ฉฐ, ์‹ค์ œ ๊ฒฝ์‚ฌ ์ธก์ •์€ ๋‹ค์Œ๊ณผ ๊ฐ™์ด ์ด๋ค„์ง€๊ฒŒ ๋œ๋‹ค. If the distance between the upper and lower wheels 22a and 22b in the moving part 20 is 50 cm, for example, the minimum measuring interval is 50 cm, and the actual inclination measurement is made as follows.
์ฆ‰, ๋„ 2์˜ (a)์— ๋„์‹œ๋œ ๋ฐ”์™€ ๊ฐ™์ด, ์ด๋™๋ถ€(20)๋ฅผ A1->B1->C1->D1->E1 ์˜ ์ˆœ์„œ๋กœ ์ด๋™์‹œํ‚ค๋ฉด์„œ ๊ฐ๋„์˜ ๋ณ€ํ™”๋ฅผ ์ธก์ •ํ•˜๋Š”๋ฐ, A1 ์ง€์ ์—์„œ ์ธก์ •์„ ํ•œ ํ›„, ์ด๋™๋ถ€(20)๋ฅผ B1 ์ง€์ ์œผ๋กœ ์ด๋™์‹œํ‚ค๋ฉด ์ตœ์ดˆ ์ธก์ •์‹œ์˜ ์ƒ๋ถ€ ๋ฐ”ํ€ด(22a)์˜ ์œ„์น˜์— ๋‘๋ฒˆ์งธ ์ธก์ •์‹œ์˜ ํ•˜๋ถ€ ๋ฐ”ํ€ด(22b)๊ฐ€ ์˜ค๊ฒŒ ๋˜์–ด ๊ทธ ์ (๊ธฐ์ค€์ )์„ ๊ธฐ์ค€์œผ๋กœ ๋‘๋ฒˆ์งธ ๊ฒฝ์‚ฌ ์ธก์ •์ด ์ด๋ฃจ์–ด์ง€๊ฒŒ ๋˜๊ณ , ์ด๋Ÿฌํ•œ ๊ณผ์ •์„ ๋ฐ˜๋ณตํ•˜์—ฌ ์ „์ฒด ๊ฒฝ์‚ฌ๊ด€ ๋‚ด์˜ ๊ฒฝ์‚ฌ๋ณ€์œ„๋ฅผ ์ธก์ •ํ•˜๊ฒŒ ๋œ๋‹ค. That is, as shown in (a) of FIG. 2, the change of the angle is measured while moving the moving part 20 in the order of A1-> B1-> C1-> D1-> E1. After moving the moving part 20 to the B1 point, the lower wheel 22b at the time of the second measurement comes to the position of the upper wheel 22a at the time of the first measurement, and the second inclination measurement is performed based on the point (reference point). This process is repeated to measure the inclination displacement in the entire inclined tube.
๋„ 2์˜ (b)์— ๋„์‹œ๋œ ๋ฐ”์™€ ๊ฐ™์ด, 50cm ์ด์ƒ์˜ ๊ฑฐ๋ฆฌ๋ฅผ ์ด๋™์‹œํ‚ค๋ฉด์„œ ๊ฒฝ์‚ฌ๋ฅผ ์ธก์ •ํ•˜๋Š” ๊ฒฝ์šฐ์—๋Š” ๊ธฐ์ค€์ ์ด ๋‹ฌ๋ผ์ง€๊ฒŒ ๋˜์–ด, x,y ๋ฐฉํ–ฅ์œผ๋กœ ๋งค์šฐ ํฐ ์ธก์ •์˜ค์ฐจ๊ฐ€ ๋ฐœ์ƒํ•  ์ˆ˜ ์žˆ๋‹ค. As shown in (b) of FIG. 2, when measuring the inclination while moving a distance of 50cm or more, the reference point is changed, a very large measurement error may occur in the x, y direction.
์ด์™€ ๊ฐ™์€ ๋ฐฉ์‹์„ ์ทจํ•˜๋Š” ์ข…๋ž˜์˜ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜๋Š” ๋‹ค์Œ๊ณผ ๊ฐ™์€ ํ•œ๊ณ„๋ฅผ ์ง€๋‹ ์ˆ˜ ๋ฐ–์— ์—†์—ˆ๋‹ค. The conventional ground displacement measuring apparatus using this method had the following limitations.
1) 2์ถ•(x,y)์˜ ๊ฒฝ์‚ฌ๋„๋งŒ ์ธก์ •ํ•˜๋ฉฐ ์ด๋™๋ถ€์˜ ์ƒํ•˜ ๋ฐ”ํ€ด ๊ฐ„๊ฒฉ์— ํ•ด๋‹นํ•˜๋Š” ์ตœ์†Œ ์ธก์ • ๊ฐ„๊ฒฉ(์œ„ ์˜ˆ์—์„œ๋Š” 50cm)์„ ๊ฐ–๊ณ  ์žˆ๊ธฐ ๋•Œ๋ฌธ์—, ๊ทธ ์ดํ•˜์˜ ๊ณก๋ฅ ๋ฐ˜๊ฒฝ์„ ์ง€๋‹ˆ๋Š” ๊ธ‰๊ฒฉํ•˜๊ณ  ๋ฏธ์„ธํ•œ ๊ฒฝ์‚ฌ์˜ ์ธก์ •์€ ๋ถˆ๊ฐ€๋Šฅํ•˜๋‹ค.1) Since only the inclination of the two axes (x, y) is measured and it has a minimum measurement interval (50 cm in the above example) corresponding to the distance between the upper and lower wheels of the moving part, the measurement of the sharp and minute inclination with the curvature radius of less than impossible.
2) ์ด๋™๋ถ€์˜ ๊ธธ์ด๊ฐ€ ์ผ์ • ๊ธธ์ด(์œ„ ์˜ˆ์—์„œ๋Š” 50cm) ์ด์ƒ์˜ ๊ฐ’์„ ๊ฐ€์ ธ์•ผ ํ•˜๋ฏ€๋กœ ๊ธ‰๊ฒฉํ•œ ๊ฒฝ์‚ฌ์—๋Š” ์ด๋™๋ถ€์˜ ํˆฌ์ž…์ด ๋ถˆ๊ฐ€๋Šฅํ•˜๋‹ค.2) Since the length of the moving part must have a value equal to or more than a predetermined length (50 cm in the above example), it is impossible to insert the moving part on a sharp slope.
3) ์ตœ์†Œ ์ธก์ • ๊ฐ„๊ฒฉ์— ๋งž์ถ”์–ด ์ด๋™์‹œํ‚ค๋ฉด์„œ ๊ฒฝ์‚ฌ๋„๋ฅผ ์ธก์ •ํ•  ๊ฒฝ์šฐ(๋„ 2์˜ (a)), ๊ธฐ์ค€์ ์˜ ๋ฏธ์„ธํ•œ ๋ถˆ์ผ์น˜๋กœ ์ธํ•ด ์ธก์ •์˜ค์ฐจ๊ฐ€ ๋ฐœ์ƒํ•œ๋‹ค.3) When measuring the inclination while moving to the minimum measurement interval (Fig. 2 (a)), a measurement error occurs due to the minute mismatch of the reference point.
4) ์ตœ์†Œ ์ธก์ • ๊ฐ„๊ฒฉ ์ด์ƒ์˜ ๊ฐ„๊ฒฉ์œผ๋กœ ์ด๋™์‹œํ‚ค๋ฉด์„œ ๊ฒฝ์‚ฌ๋„๋ฅผ ์ธก์ •ํ•  ๊ฒฝ์šฐ(๋„ 2์˜ (b)), ๊ธฐ์ค€์ ์˜ ๋ถˆ์ผ์น˜๋กœ x,y ๋ฐฉํ–ฅ์˜ ์˜ค์ฐจ๊ฐ€ ๋ฐœ์ƒํ•œ๋‹ค.4) In the case of measuring the inclination while moving at an interval greater than the minimum measurement interval (Fig. 2 (b)), the misalignment of the reference point causes errors in the x, y direction.
5) ๊ฐ ์ธก์ • ์ง€์ ์—์„œ์˜ ๊ฒฝ์‚ฌ๋„๋งŒ์„ ์ธก์ •ํ•˜์—ฌ ๋ณ€์œ„๋Ÿ‰์„ ๊ณ„์‚ฐํ•˜๋ฏ€๋กœ, ์ฒœ๊ณต์ˆ˜์ง๋„ ํ˜น์€ ๊ฒฝ์‚ฌ๊ด€์˜ ๋น„ํ‹€๋ฆผ์ด ๋ฐœ์ƒํ•  ๊ฒฝ์šฐ ์ƒ๋‹นํ•œ ์ธก์ •์˜ค์ฐจ๊ฐ€ ๋ฐœ์ƒํ•œ๋‹ค.5) Since the displacement is calculated by measuring only the inclination at each measurement point, a significant measurement error occurs in the case of perforation verticality or torsion of the inclined pipe.
6) ์‹ค์ œ ์ธก์ •๊ณผ์ •์— ์žˆ์–ด์„œ ์ธก์ •ํ•˜๋Š” ์‚ฌ๋žŒ๊ณผ ๋ฐฉ๋ฒ•์— ๋”ฐ๋ผ ๊ฒฐ๊ณผ๊ฐ€ ๋‹ฌ๋ผ์งˆ ๊ฐ€๋Šฅ์„ฑ์ด ๋†’๊ธฐ ๋•Œ๋ฌธ์— ๋ฐ์ดํ„ฐ์˜ ๊ฐ๊ด€์„ฑ์ด ๋–จ์–ด์ง€๊ฒŒ ๋œ๋‹ค. 6) In the actual measurement process, the objectivity of the data decreases because the results are likely to vary depending on the measuring person and the method.
๋ณธ ๋ฐœ๋ช…์€ ์ƒ๊ธฐ์™€ ๊ฐ™์€ ๋ฌธ์ œ์ ์„ ๊ฐ์•ˆํ•˜์—ฌ ์•ˆ์ถœํ•œ ๊ฒƒ์œผ๋กœ์„œ, ์ง€๋ฐ˜์— ์ˆ˜์ง์œผ๋กœ ๊ตด์ฐฉ๋œ ๊ฒฝ์‚ฌ๊ด€์— ์‚ฝ์ž…๋˜์–ด ๊ทธ ๊ธธ์ด๋ฐฉํ–ฅ์œผ๋กœ ์ด๋™ํ•˜๋ฉด์„œ ์ ‘์ด‰์‹์œผ๋กœ ์ง€๋ฐ˜ ๋ณ€์œ„๋ฅผ ๊ฐ์ง€ํ•˜๋˜, ์„ค์ •๋œ ์ธก์ • ํƒ€์ด๋ฐ์— ๋งž์ถฐ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„๋ฅผ ์‹ค์‹œ๊ฐ„์œผ๋กœ ์ธก์ •ํ•˜๋„๋ก ๊ตฌ์„ฑ๋œ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜๋ฅผ ์ œ๊ณตํ•˜๋Š” ๊ฒƒ์„ ๊ทธ ๋ชฉ์ ์œผ๋กœ ํ•œ๋‹ค. The present invention has been made in view of the above problems, it is inserted into the inclined tube excavated perpendicular to the ground and moved in its longitudinal direction to detect the ground displacement by contact, but the three-dimensional coordinate displacement in accordance with the set measurement timing It is an object of the present invention to provide a ground displacement measuring device configured to measure in real time.
ํŠนํžˆ ๋ณธ ๋ฐœ๋ช…์€, ๋‹ค์–‘ํ•œ ์„ผ์„œ ์กฐํ•ฉ์„ ์ด์šฉํ•˜๊ฑฐ๋‚˜ ๋ณต์ˆ˜์˜ ์ธก์ • ํƒ€์ด๋ฐ์„ ์„ค์ •ํ•˜์—ฌ ์ธก์ • ๋ฐ์ดํ„ฐ์— ๋Œ€ํ•œ ๋‹ค์–‘ํ•œ ๋ณด์ • ์ฒ˜๋ฆฌ๊ฐ€ ์ด๋ค„์ง€๋„๋ก ํ•˜์—ฌ, ์ธก์ • ๊ธฐ์ค€์ ์˜ ๋ถˆ์ผ์น˜ ๋˜๋Š” ์ฒœ๊ณต์ˆ˜์ง๋„, ๊ฒฝ์‚ฌ๊ด€ ๋น„ํ‹€๋ฆผ ๋“ฑ์œผ๋กœ ๋ฐœ์ƒํ–ˆ๋˜ ์ข…๋ž˜์˜ ์ธก์ •์˜ค์ฐจ ๋ฌธ์ œ๋ฅผ ํ•ด๊ฒฐํ•˜๋Š” ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜๋ฅผ ์ œ๊ณตํ•˜๋Š” ๊ฒƒ์„ ๋˜๋‹ค๋ฅธ ๋ชฉ์ ์œผ๋กœ ํ•œ๋‹ค. In particular, the present invention, by using a variety of sensor combinations or by setting a plurality of measurement timings to perform a variety of correction processing for the measurement data, the conventional measurement error caused by mismatch of measurement reference point or puncture verticality, inclination of the inclined pipe It is another object to provide a ground displacement measuring device that solves the problem.
๋˜ํ•œ ๋ณธ ๋ฐœ๋ช…์€, ์ด๋™๋ถ€์˜ ๊ธธ์ด๋ฅผ ์ข…๋ž˜์— ๋น„ํ•ด ์ž‘๊ฒŒ ์ œ์ž‘ํ•  ์ˆ˜ ์žˆ์–ด, ์ข…๋ž˜ ์ด๋™๋ถ€์˜ ์ƒํ•˜ ๋ฐ”ํ€ด ๊ฐ„๊ฒฉ ์ดํ•˜์˜ ๊ณก๋ฅ ๋ฐ˜๊ฒฝ์„ ์ง€๋‹ˆ๋Š” ๊ธ‰๊ฒฉํ•˜๊ณ  ๋ฏธ์„ธํ•œ ๊ฒฝ์‚ฌ๋„ ์ •๋ฐ€ํ•˜๊ฒŒ ์ธก์ •ํ•  ์ˆ˜ ์žˆ์œผ๋ฉฐ, ๊ธ‰๊ฒฉํ•œ ๊ฒฝ์‚ฌ์—๋„ ์ด๋™๋ถ€์˜ ํˆฌ์ž…์ด ๊ฐ€๋Šฅํ•œ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜๋ฅผ ์ œ๊ณตํ•˜๋Š” ๊ฒƒ์„ ๋˜๋‹ค๋ฅธ ๋ชฉ์ ์œผ๋กœ ํ•œ๋‹ค. In addition, the present invention can make the length of the moving portion smaller than the conventional, can accurately measure the sharp and minute inclination having a radius of curvature less than the vertical wheel spacing of the conventional moving portion, and the ground displacement that can be added to the moving portion even in a sharp slope It is another object to provide a measuring device.
์ƒ๊ธฐ์™€ ๊ฐ™์€ ๋ชฉ์ ์„ ๋‹ฌ์„ฑํ•˜๊ธฐ ์œ„ํ•œ ๋ณธ ๋ฐœ๋ช…์˜ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜๋Š”, ์ง€๋ฐ˜์— ์ˆ˜์ง์œผ๋กœ ๊ตด์ฐฉ๋œ ๊ฒฝ์‚ฌ๊ด€์— ์‚ฝ์ž…๋˜์–ด ๊ทธ ๊ธธ์ด๋ฐฉํ–ฅ์œผ๋กœ ์ด๋™ ๊ฐ€๋Šฅํ•˜๋ฉฐ, ๊ฒฝ์‚ฌ๊ด€ ๋‚ด๋ฉด์˜ ๋ณ€์œ„๋ฅผ ์ ‘์ด‰์‹์œผ๋กœ ๊ฐ์ง€ํ•˜๋Š” ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜๋กœ์„œ, ๊ฒฝ์‚ฌ๊ด€ ๋‚ด์—์„œ ๊ทธ ๊ธธ์ด๋ฐฉํ–ฅ์œผ๋กœ ์ด๋™์‹œ ์ธก์ • ํƒ€์ด๋ฐ๋งˆ๋‹ค 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„๋ฅผ ์ธก์ •ํ•˜๋Š” ์„ผ์‹ฑ์ˆ˜๋‹จ; ์ƒ๊ธฐ ์ธก์ • ํƒ€์ด๋ฐ์„ ์„ค์ •ํ•˜๋Š” ํƒ€์ด๋ฐ์„ค์ •์ˆ˜๋‹จ; ์ƒ๊ธฐ ์„ผ์‹ฑ์ˆ˜๋‹จ์—์„œ ์ธก์ •ํ•œ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„ ๋ฐ์ดํ„ฐ๋ฅผ ์ง€๋ฐ˜๋ณ€์œ„๋Ÿ‰์œผ๋กœ ์—ฐ์‚ฐํ•˜๋Š” ๋ณ€์œ„๋Ÿ‰์—ฐ์‚ฐ์ˆ˜๋‹จ; ์„ ํฌํ•จํ•˜์—ฌ ๊ตฌ์„ฑ๋œ๋‹ค. The ground displacement measuring apparatus of the present invention for achieving the above object is inserted into the inclined tube vertically excavated to the ground is movable in the longitudinal direction, the ground displacement measurement to detect the displacement of the inner surface of the inclined tube by contact type An apparatus, comprising: sensing means for measuring a three-dimensional coordinate displacement at every measurement timing when moving in its longitudinal direction in an inclined tube; Timing setting means for setting the measurement timing; Displacement amount calculation means for calculating three-dimensional coordinate displacement data measured by the sensing means as ground displacement; It is configured to include.
๋ณด๋‹ค ๋ฐ”๋žŒ์งํ•˜๊ฒŒ, ์ƒ๊ธฐ ์„ผ์‹ฑ์ˆ˜๋‹จ์€ 3์ถ• ์Ÿˆ์ด๋กœ์„ผ์„œ ๋˜๋Š” 3์ถ• ๊ฐ€์†๋„์„ผ์„œ ์ค‘์˜ ์–ด๋Š ํ•˜๋‚˜๋กœ ๊ตฌ์„ฑ๋œ๋‹ค. More preferably, the sensing means is composed of any one of a three-axis gyro sensor or a three-axis acceleration sensor.
๋ณธ ๋ฐœ๋ช…์˜ ๋˜๋‹ค๋ฅธ ๊ด€์ ์—์„œ, ์ƒ๊ธฐ ์„ผ์‹ฑ์ˆ˜๋‹จ์€ 2์ถ• ์Ÿˆ์ด๋กœ์„ผ์„œ ๋˜๋Š” 2์ถ• ๊ฐ€์†๋„์„ผ์„œ ์ค‘์˜ ์–ด๋Š ํ•˜๋‚˜์™€ ์ง€๋ฐ˜ ์ˆ˜์ง๋ฐฉํ–ฅ ์ด๋™๊ฑฐ๋ฆฌ ์ธก์ •์„ผ์„œ์˜ ์กฐํ•ฉ์œผ๋กœ ์ด๋ค„์ง„๋‹ค. In another aspect of the present invention, the sensing means consists of a combination of either a two-axis gyro sensor or two-axis acceleration sensor and the ground vertical movement distance measuring sensor.
๋ณด๋‹ค ๋ฐ”๋žŒ์งํ•˜๊ฒŒ, ์ƒ๊ธฐ ์„ผ์‹ฑ์ˆ˜๋‹จ์€ ์ƒํ˜ธ ๋…๋ฆฝ์ ์ธ ์ธก์ •๋ฐฉ์‹์„ ๊ฐ–๋Š” ๋ณต์ˆ˜์˜ ์„ผ์‹ฑ์ˆ˜๋‹จ์œผ๋กœ ๊ตฌ์„ฑ๋˜๋ฉฐ, ์ƒ๊ธฐ ๊ฐ ์„ผ์‹ฑ์ˆ˜๋‹จ์ด ์ธก์ •ํ•œ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„ ๋ฐ์ดํ„ฐ๋ฅผ ์ƒํ˜ธ ๋น„๊ตํ•˜์—ฌ ๋ณด์ •ํ•˜๋Š” ๊ธฐ๋Šฅ์„ ๊ตฌ๋น„ํ•œ๋‹ค. More preferably, the sensing means is composed of a plurality of sensing means having a mutually independent measuring method, and has a function of comparing and correcting the three-dimensional coordinate displacement data measured by each sensing means.
๋ณด๋‹ค ๋ฐ”๋žŒ์งํ•˜๊ฒŒ, ์ƒ๊ธฐ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„ ๋ฐ์ดํ„ฐ์˜ ์ƒํ˜ธ ๋น„๊ต ๋ฐ ๋ณด์ •์€, ์ผ์ธก ์„ผ์‹ฑ์ˆ˜๋‹จ์ด ์ธก์ •ํ•œ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„ ๋ฐ์ดํ„ฐ๋ฅผ ๊ธฐ์ค€์œผ๋กœ, ํƒ€์ธก ์„ผ์‹ฑ์ˆ˜๋‹จ์ด ์ธก์ •ํ•œ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„ ๋ฐ์ดํ„ฐ ์ค‘ ๊ธฐ์„ค์ •๋œ ์˜ค์ฐจ๋ฒ”์œ„๋ฅผ ๋„˜์–ด์„œ๋Š” ๊ฐ’์„ ๋‚˜ํƒ€๋‚ธ ๊ฒฝ์šฐ๋ฅผ ์—๋Ÿฌ๋กœ ํŒ๋‹จํ•˜์—ฌ ์ฒ˜๋ฆฌํ•˜๋„๋ก ๊ตฌ์„ฑ๋œ๋‹ค. More preferably, the mutual comparison and correction of the three-dimensional coordinate displacement data, based on the three-dimensional coordinate displacement data measured by one side sensing means, exceeding a predetermined error range of the three-dimensional coordinate displacement data measured by the other sensing means. The case where the value is indicated is determined to be an error and is processed.
๋ณด๋‹ค ๋ฐ”๋žŒ์งํ•˜๊ฒŒ, ์ƒ๊ธฐ ๋ณต์ˆ˜์˜ ์„ผ์‹ฑ์ˆ˜๋‹จ์€ ์ ์–ด๋„ 2๊ฐœ์˜ ์„ผ์„œ๋กœ ๊ตฌ์„ฑ๋˜๋ฉฐ, 3์ถ• ์Ÿˆ์ด๋กœ์„ผ์„œ์™€ 3์ถ• ๊ฐ€์†๋„์„ผ์„œ๋ฅผ ํฌํ•จํ•œ๋‹ค. More preferably, the plurality of sensing means includes at least two sensors, and includes a three-axis gyro sensor and a three-axis acceleration sensor.
๋ณธ ๋ฐœ๋ช…์˜ ๋˜๋‹ค๋ฅธ ๊ด€์ ์—์„œ, ์ƒ๊ธฐ ๋ณต์ˆ˜์˜ ์„ผ์‹ฑ์ˆ˜๋‹จ์€ ์ ์–ด๋„ 2๊ฐœ์˜ ์„ผ์„œ ์กฐํ•ฉ์œผ๋กœ ๊ตฌ์„ฑ๋˜๋ฉฐ, ์ƒ๊ธฐ ์„ผ์„œ ์กฐํ•ฉ์€ 2์ถ• ์Ÿˆ์ด๋กœ์„ผ์„œ์™€ ์ง€๋ฐ˜ ์ˆ˜์ง๋ฐฉํ–ฅ ์ด๋™๊ฑฐ๋ฆฌ ์ธก์ •์„ผ์„œ์˜ ์กฐํ•ฉ๊ณผ 2์ถ• ๊ฐ€์†๋„์„ผ์„œ์™€ ์ง€๋ฐ˜ ์ˆ˜์ง๋ฐฉํ–ฅ ์ด๋™๊ฑฐ๋ฆฌ ์ธก์ •์„ผ์„œ์˜ ์กฐํ•ฉ์„ ํฌํ•จํ•œ๋‹ค. In another aspect of the invention, the plurality of sensing means is composed of at least two sensor combinations, the sensor combinations are a combination of a 2-axis gyro sensor and a ground vertical travel distance measurement sensor and a 2-axis acceleration sensor and ground vertical A combination of directional travel distance sensors.
๋ณด๋‹ค ๋ฐ”๋žŒ์งํ•˜๊ฒŒ ๋ณธ ๋ฐœ๋ช…์€, ์ง€๋ฐ˜ ์ˆ˜์ง๋ฐฉํ–ฅ ์ด๋™๊ฑฐ๋ฆฌ ์ธก์ •์„ผ์„œ ๋˜๋Š” ์˜จ๋„์„ผ์„œ ์ค‘์˜ ์ ์–ด๋„ ์–ด๋Š ํ•˜๋‚˜๋ฅผ ๋ณด์กฐ ์„ผ์‹ฑ์ˆ˜๋‹จ์œผ๋กœ ๋” ๊ตฌ๋น„ํ•˜์—ฌ, ์ƒ๊ธฐ ์„ผ์‹ฑ์ˆ˜๋‹จ์ด ์ธก์ •ํ•œ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„ ๋ฐ์ดํ„ฐ๋ฅผ ๋ณด์ •ํ•˜๋Š” ๊ธฐ๋Šฅ์„ ๊ตฌ๋น„ํ•œ๋‹ค.More preferably, the present invention further includes at least one of a ground vertical movement distance measuring sensor and a temperature sensor as auxiliary sensing means, and has a function of correcting three-dimensional coordinate displacement data measured by the sensing means.
๋ณธ ๋ฐœ๋ช…์˜ ๋˜๋‹ค๋ฅธ ๊ด€์ ์—์„œ, ์ƒ๊ธฐ ํƒ€์ด๋ฐ์„ค์ •์ˆ˜๋‹จ์€ ์ƒํ˜ธ ๋…๋ฆฝ์ ์ธ ๋ณต์ˆ˜์˜ ์ฃผํŒŒ์ˆ˜๋ฅผ ์ธก์ • ํƒ€์ด๋ฐ์œผ๋กœ ์„ค์ •ํ•  ์ˆ˜ ์žˆ๋„๋ก ๊ตฌ๋น„๋˜์–ด, ๊ฐ ์ฃผํŒŒ์ˆ˜๋ณ„๋กœ ์ƒ๊ธฐ ์„ผ์‹ฑ์ˆ˜๋‹จ์ด ์ธก์ •ํ•œ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„ ๋ฐ์ดํ„ฐ๋ฅผ ์ƒํ˜ธ ๋น„๊ตํ•˜์—ฌ ๋ณด์ •ํ•˜๋Š” ๊ธฐ๋Šฅ์„ ๊ตฌ๋น„ํ•œ๋‹ค. In another aspect of the present invention, the timing setting means is provided to set a plurality of mutually independent frequencies as the measurement timing, the function of comparing and correcting the three-dimensional coordinate displacement data measured by the sensing means for each frequency It is provided.
๋ณธ ๋ฐœ๋ช…์˜ ๋˜๋‹ค๋ฅธ ๊ด€์ ์—์„œ, ์ƒ๊ธฐ ์„ผ์‹ฑ์ˆ˜๋‹จ์€ ๋ณต์ˆ˜์˜ ์„ผ์‹ฑ์ˆ˜๋‹จ์œผ๋กœ ๊ตฌ์„ฑ๋˜๋ฉฐ, ์ƒ๊ธฐ ํƒ€์ด๋ฐ์„ค์ •์ˆ˜๋‹จ์€ ๊ฐ ์„ผ์‹ฑ์ˆ˜๋‹จ๋ณ„๋กœ ์ƒํ˜ธ ๋…๋ฆฝ์ ์ธ ๋ณต์ˆ˜์˜ ์ฃผํŒŒ์ˆ˜๋ฅผ ์ธก์ • ํƒ€์ด๋ฐ์œผ๋กœ ์„ค์ •ํ•  ์ˆ˜ ์žˆ๋„๋ก ๊ตฌ๋น„๋˜์–ด, ์ƒ๊ธฐ ๊ฐ ์„ผ์‹ฑ์ˆ˜๋‹จ์ด ์ธก์ •ํ•œ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„ ๋ฐ์ดํ„ฐ๋ฅผ ์ƒํ˜ธ ๋น„๊ตํ•˜์—ฌ ๋ณด์ •ํ•˜๋Š” ๊ธฐ๋Šฅ์„ ๊ตฌ๋น„ํ•œ๋‹ค. In another aspect of the present invention, the sensing means is composed of a plurality of sensing means, the timing setting means is provided to set a plurality of frequencies independent of each sensing means for each of the sensing means, each of the sensing means And a function of comparing and correcting the measured three-dimensional coordinate displacement data with each other.
๋ณด๋‹ค ๋ฐ”๋žŒ์งํ•˜๊ฒŒ, ์ƒ๊ธฐ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„ ๋ฐ์ดํ„ฐ์˜ ์ƒํ˜ธ ๋น„๊ต ๋ฐ ๋ณด์ •์€, ํ•˜๋‚˜์˜ ์ฃผํŒŒ์ˆ˜๋ฅผ ์ธก์ • ํƒ€์ด๋ฐ์œผ๋กœ ์„ค์ •ํ•˜์—ฌ ์ธก์ •ํ•œ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„ ๋ฐ์ดํ„ฐ๋ฅผ ๊ธฐ์ค€์œผ๋กœ, ๋˜๋‹ค๋ฅธ ์ฃผํŒŒ์ˆ˜๋ฅผ ์ธก์ • ํƒ€์ด๋ฐ์œผ๋กœ ์„ค์ •ํ•˜์—ฌ ์ธก์ •ํ•œ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„ ๋ฐ์ดํ„ฐ ์ค‘ ๊ธฐ์„ค์ •๋œ ์˜ค์ฐจ๋ฒ”์œ„๋ฅผ ๋„˜์–ด์„œ๋Š” ๊ฐ’์„ ๋‚˜ํƒ€๋‚ธ ๊ฒฝ์šฐ๋ฅผ ์—๋Ÿฌ๋กœ ํŒ๋‹จํ•˜์—ฌ ์ฒ˜๋ฆฌํ•˜๋„๋ก ๊ตฌ์„ฑ๋œ๋‹ค. More preferably, the mutual comparison and correction of the three-dimensional coordinate displacement data is based on the three-dimensional coordinate displacement data measured by setting one frequency as the measurement timing, and the three-dimensional measured by setting another frequency as the measurement timing. It is configured to determine and process a case in which a value exceeding a preset error range among coordinate displacement data is regarded as an error.
๋ณธ ๋ฐœ๋ช…์˜ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜๋Š”, ์ด๋™๋ถ€๊ฐ€ ๊ฒฝ์‚ฌ๊ด€ ๋‚ด ์ด๋™ ์ค‘์— ์ธก์ • ํƒ€์ด๋ฐ์— ๋งž์ถฐ ์‹ค์‹œ๊ฐ„์œผ๋กœ 3์ฐจ์›(๋˜๋Š” 3์ถ•) ๋ฐฉํ–ฅ์˜ ๋ณ€์œ„๋ฅผ ์ธก์ •ํ•˜๊ธฐ ๋•Œ๋ฌธ์—, ์ตœ์†Œ ์ธก์ • ๊ฐ„๊ฒฉ์ด๋‚˜ ๊ธฐ์ค€์  ๋“ฑ์„ ๊ณ ๋ คํ•  ํ•„์š” ์—†์ด ์ธก์ • ๊ณผ์ •์ด ์ด๋ค„์ง€๊ฒŒ ๋˜์–ด ๊ธฐ์ค€์ ์˜ ๋ถˆ์ผ์น˜ ๋˜๋Š” ์ฒœ๊ณต์ˆ˜์ง๋„, ๊ฒฝ์‚ฌ๊ด€ ๋น„ํ‹€๋ฆผ ๋“ฑ์œผ๋กœ ๋ฐœ์ƒํ–ˆ๋˜ ์ข…๋ž˜์˜ ์ธก์ •์˜ค์ฐจ ๋ฌธ์ œ๋ฅผ ํ•ด๊ฒฐํ•ด ์ค€๋‹ค. In the ground displacement measuring apparatus of the present invention, since the moving unit measures the displacement in the three-dimensional (or three-axis) direction in real time according to the measurement timing during the movement in the inclined tube, the measurement process is not necessary without considering the minimum measurement interval or reference point. This solves the conventional measurement error problem caused by the mismatch of the reference point or the perforated vertical degree, the inclination of the inclined tube.
๋˜ํ•œ, ์ด๋™๋ถ€์˜ ๊ธธ์ด๋ฅผ ์ข…๋ž˜์— ๋น„ํ•ด ์ž‘๊ฒŒ ์ œ์ž‘ํ•  ์ˆ˜ ์žˆ์œผ๋ฏ€๋กœ, ์ด๋™๋ถ€์˜ ์ƒํ•˜ ๋ฐ”ํ€ด ๊ฐ„๊ฒฉ ์ดํ•˜์˜ ๊ณก๋ฅ ๋ฐ˜๊ฒฝ์„ ์ง€๋‹ˆ๋Š” ๊ธ‰๊ฒฉํ•˜๊ณ  ๋ฏธ์„ธํ•œ ๊ฒฝ์‚ฌ๋„ ์ •๋ฐ€ํ•˜๊ฒŒ ์ธก์ •ํ•  ์ˆ˜ ์žˆ์œผ๋ฉฐ, ๊ธ‰๊ฒฉํ•œ ๊ฒฝ์‚ฌ์—๋„ ์ด๋™๋ถ€์˜ ํˆฌ์ž…์ด ๊ฐ€๋Šฅํ•œ ์žฅ์ ์ด ์žˆ๋‹ค. In addition, since the length of the moving part can be made smaller than in the related art, a sharp and minute inclination having a radius of curvature of the upper and lower wheel intervals of the moving part can be accurately measured, and there is an advantage that the moving part can be inserted even in a sharp inclination.
๋˜ํ•œ, ์ธก์ •ํ•˜๋Š” ์‚ฌ๋žŒ๊ณผ ๋ฐฉ๋ฒ•์— ๋”ฐ๋ฅธ ์ธก์ •์˜ค์ฐจ ๋ฌธ์ œ๋„ ํ•ด๊ฒฐํ•˜๊ธฐ ๋•Œ๋ฌธ์—, ๋ฐ์ดํ„ฐ์˜ ๊ฐ๊ด€์„ฑ๊ณผ ์ •๋ฐ€๋„๋ฅผ ํ–ฅ์ƒ์‹œํ‚ค๋Š” ์žฅ์ ์„ ์ œ๊ณตํ•œ๋‹ค.In addition, it solves the measurement error problem according to the person and the method of measurement, thereby providing the advantage of improving the objectivity and precision of the data.
๋˜ํ•œ, ๋‹ค์–‘ํ•œ ์„ผ์„œ ์กฐํ•ฉ์„ ์ด์šฉํ•˜๊ฑฐ๋‚˜ ๋ณต์ˆ˜์˜ ์ธก์ • ํƒ€์ด๋ฐ์„ ์„ค์ •ํ•˜์—ฌ ์ธก์ • ๋ฐ์ดํ„ฐ์— ๋Œ€ํ•œ ๋‹ค์–‘ํ•œ ๋ณด์ • ์ฒ˜๋ฆฌ๋ฅผ ํ•˜๋ฏ€๋กœ, ์ธก์ •์˜ค์ฐจ๋ฅผ ์ตœ๋Œ€ํ•œ ์ค„์ด๋Š” ์žฅ์ ์„ ์ œ๊ณตํ•œ๋‹ค. In addition, since various correction processing is performed on the measurement data by using various sensor combinations or by setting a plurality of measurement timings, the measurement error is reduced as much as possible.
๋„ 1์€ ์ข…๋ž˜์˜ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜์˜ ์ผ์˜ˆ๋ฅผ ๋‚˜ํƒ€๋‚ธ ๊ตฌ์„ฑ๋„,1 is a configuration diagram showing an example of a conventional ground displacement measuring apparatus,
๋„ 2๋Š” ์ข…๋ž˜์˜ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜์˜ ์ธก์ •์˜ˆ๋ฅผ ๋‚˜ํƒ€๋‚ธ ์‚ฌ์šฉ์ƒํƒœ๋„, 2 is a use state diagram showing a measurement example of a conventional ground displacement measuring apparatus,
๋„ 3 ๋ฐ ๋„ 4๋Š” ๋ณธ ๋ฐœ๋ช…์˜ ์ผ์‹ค์‹œ์˜ˆ์— ์˜ํ•œ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜์˜ ๊ตฌ์„ฑ๋„, 3 and 4 is a block diagram of a ground displacement measuring apparatus according to an embodiment of the present invention,
๋„ 5๋Š” ๋ณธ ๋ฐœ๋ช…์˜ ์ผ์‹ค์‹œ์˜ˆ์— ์˜ํ•œ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜์˜ ์‚ฌ์šฉ์ƒํƒœ๋„, 5 is a state diagram used in the ground displacement measuring apparatus according to an embodiment of the present invention,
๋„ 6์€ ๋ณธ ๋ฐœ๋ช…์˜ ์ผ์‹ค์‹œ์˜ˆ์— ์˜ํ•œ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜์˜ ์ž‘๋™ํ๋ฆ„๋„,6 is an operation flow chart of the ground displacement measuring apparatus according to an embodiment of the present invention,
๋„ 7์€ ๋ณธ ๋ฐœ๋ช…์˜ ๋˜๋‹ค๋ฅธ ์‹ค์‹œ์˜ˆ์— ์˜ํ•œ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜์˜ ์ž‘๋™ํ๋ฆ„๋„,7 is an operation flow chart of the ground displacement measuring apparatus according to another embodiment of the present invention,
๋„ 8์€ ๋ณธ ๋ฐœ๋ช…์˜ ๋˜๋‹ค๋ฅธ ์‹ค์‹œ์˜ˆ์— ์˜ํ•œ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜์˜ ๊ตฌ์„ฑ๋„, 8 is a block diagram of a ground displacement measuring apparatus according to another embodiment of the present invention,
๋„ 9๋Š” ๋ณธ ๋ฐœ๋ช…์˜ ๋˜๋‹ค๋ฅธ ์‹ค์‹œ์˜ˆ์— ์˜ํ•œ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜์˜ ์ž‘๋™ํ๋ฆ„๋„,9 is an operation flow chart of the ground displacement measuring apparatus according to another embodiment of the present invention,
๋„ 10์€ ๋ณธ ๋ฐœ๋ช…์˜ ๋˜๋‹ค๋ฅธ ์‹ค์‹œ์˜ˆ์— ์˜ํ•œ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜์˜ ๊ตฌ์„ฑ๋„, 10 is a block diagram of a ground displacement measuring apparatus according to another embodiment of the present invention,
๋„ 11์€ ๋ณธ ๋ฐœ๋ช…์˜ ๋˜๋‹ค๋ฅธ ์‹ค์‹œ์˜ˆ์— ์˜ํ•œ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜์˜ ์ž‘๋™ํ๋ฆ„๋„,11 is an operation flow chart of the ground displacement measuring apparatus according to another embodiment of the present invention,
๋„ 12๋Š” ๋ณธ ๋ฐœ๋ช…์˜ ๋˜๋‹ค๋ฅธ ์‹ค์‹œ์˜ˆ์— ์˜ํ•œ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜์˜ ๊ตฌ์„ฑ๋„, 12 is a block diagram of a ground displacement measuring apparatus according to another embodiment of the present invention,
๋„ 13์€ ๋ณธ ๋ฐœ๋ช…์˜ ๋˜๋‹ค๋ฅธ ์‹ค์‹œ์˜ˆ์— ์˜ํ•œ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜์˜ ์ž‘๋™ํ๋ฆ„๋„, 13 is an operation flow chart of the ground displacement measuring apparatus according to another embodiment of the present invention,
๋„ 14๋Š” ๋ณธ ๋ฐœ๋ช…์˜ ๋˜๋‹ค๋ฅธ ์‹ค์‹œ์˜ˆ์— ์˜ํ•œ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜์˜ ์ž‘๋™ํ๋ฆ„๋„์ด๋‹ค. 14 is an operation flowchart of the ground displacement measuring apparatus according to another embodiment of the present invention.
๋„ 3 ๋ฐ ๋„ 4๋Š” ๋ณธ ๋ฐœ๋ช…์˜ ์ผ์‹ค์‹œ์˜ˆ์— ์˜ํ•œ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜์˜ ๊ตฌ์„ฑ๋„, ๋„ 5๋Š” ๋ณธ ๋ฐœ๋ช…์˜ ์ผ์‹ค์‹œ์˜ˆ์— ์˜ํ•œ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜์˜ ์‚ฌ์šฉ์ƒํƒœ๋„, ๋„ 6์€ ๋ณธ ๋ฐœ๋ช…์˜ ์ผ์‹ค์‹œ์˜ˆ์— ์˜ํ•œ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜์˜ ์ž‘๋™ํ๋ฆ„๋„์ด๋‹ค. 3 and 4 is a configuration diagram of a ground displacement measuring apparatus according to an embodiment of the present invention, Figure 5 is a state diagram of the ground displacement measuring apparatus according to an embodiment of the present invention, Figure 6 is an embodiment of the present invention This is an example of the operation flow chart of the ground displacement measuring device.
๋ณธ ์‹ค์‹œ์˜ˆ์˜ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜๋Š” ์ด๋™์‹์œผ๋กœ์„œ, ์ง€ํ•˜์— ๊ตด์ฐฉ๋œ ๊ฒฝ์‚ฌ๊ด€(500)์˜ ๋‚ด์ฃผ๋ฉด์„ ๋”ฐ๋ผ ์ˆ˜์ง ์ด๋™๋˜์–ด ์ง€๋ฐ˜์˜ ๋ณ€์œ„๋ฅผ ๊ฐ์ง€ํ•˜๋Š” ์ด๋™๋ถ€(400)์™€, ์ง€์ƒ์— ์œ„์น˜ํ•˜๋ฉฐ ์ „์„ (๋˜๋Š” ์‹ ํ˜ธ์„ , 300)์„ ํ†ตํ•ด ์—ฐ๊ฒฐ๋˜์–ด ์ด๋™๋ถ€(400)์—์„œ ์ „์†กํ•œ ์ธก์ •๊ฐ’์„ ์ด์šฉํ•˜์—ฌ ์ง€๋ฐ˜ ๋ณ€์œ„๋ฅผ ์—ฐ์‚ฐํ•˜๋Š” ์—ฐ์‚ฐ์ œ์–ด๋ถ€(200)๋ฅผ ํฌํ•จํ•˜์—ฌ ๊ตฌ์„ฑ๋œ๋‹ค. Ground displacement measuring apparatus of the present embodiment is a movable, vertical movement along the inner circumferential surface of the inclined pipe 500 excavated underground, the moving unit 400 for detecting the displacement of the ground, and located on the ground wire (or signal line, 300 It is configured to include a calculation control unit 200 connected to the through and to calculate the ground displacement using the measured value transmitted from the moving unit 400.
์ด๋™๋ถ€(400)๋Š” ํ”„๋กœ๋ธŒ(probe)๋ผ๊ณ ๋„ ํ•˜๋ฉฐ, ๋ชจํ„ฐ(410) ๋˜๋Š” ์ด์™€ ๊ท ๋“ฑํ•œ ๊ธฐ๋Šฅ์„ ์ˆ˜ํ–‰ํ•˜๋Š” ๊ณต์ง€์˜ ๊ตฌ๋™์ˆ˜๋‹จ์— ์˜ํ•ด ์ˆ˜์ง๋ฐฉํ–ฅ ์ด๋™์„ ํ•˜๊ฒŒ ๋œ๋‹ค. ์ด๋Ÿฌํ•œ ๊ตฌ๋™์ˆ˜๋‹จ์€ ์ž๋™ ๋˜๋Š” ์ˆ˜๋™๋ฐฉ์‹์„ ๋ชจ๋‘ ํฌํ•จํ•œ๋‹ค. The moving part 400 is also called a probe, and moves vertically by a motor 410 or a known driving means that performs an equivalent function. Such drive means include both automatic and manual methods.
์ด๋™๋ถ€(400)๋Š” ์™ธ์ธก์œผ๋กœ ๋Œ์ถœ๋œ ๋ณต์ˆ˜์˜ ๋ฐ”ํ€ด(410a,410b)๋ฅผ ๊ตฌ๋น„ํ•˜๋ฏ€๋กœ, ๋ชจํ„ฐ(410)์˜ ๊ตฌ๋™์‹œ ๊ฒฝ์‚ฌ๊ด€(500)์˜ ๋‚ด์ฃผ๋ฉด์„ ๋”ฐ๋ผ ์ ‘์ด‰ ์ƒํƒœ๋ฅผ ๋งŒ๋“ค๋ฉด์„œ ์ˆ˜์ง์œผ๋กœ ์Šนํ•˜๊ฐ•๋œ๋‹ค. Since the moving part 400 includes a plurality of wheels 410a and 410b protruding outward, the moving part 400 is vertically moved up and down while making a contact state along the inner circumferential surface of the inclined tube 500 when the motor 410 is driven.
์ด๋Ÿฌํ•œ ๊ตฌ์กฐ๋Š” ๋„ 1 ๋ฐ ๋„ 2๋ฅผ ํ†ตํ•ด ์„ค๋ช…ํ•œ ์ข…๋ž˜์˜ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜์™€ ์œ ์‚ฌํ•œ ๊ตฌ์กฐ๋กœ ๋ณผ ์ˆ˜๋„ ์žˆ๋‹ค. ์ฆ‰, ๋ณธ ์‹ค์‹œ์˜ˆ์˜ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜๋Š” ์ง€๋ฐ˜์— ์ˆ˜์ง์œผ๋กœ ๊ตด์ฐฉ๋œ ๊ฒฝ์‚ฌ๊ด€(500)์— ์‚ฝ์ž…๋˜์–ด ๊ทธ ๊ธธ์ด๋ฐฉํ–ฅ(z๋ฐฉํ–ฅ)์œผ๋กœ ์ด๋™ ๊ฐ€๋Šฅํ•˜๋ฉฐ ๊ฒฝ์‚ฌ๊ด€ ๋‚ด๋ฉด์˜ ๋ณ€์œ„๋ฅผ ์ ‘์ด‰์‹์œผ๋กœ ๊ฐ์ง€ํ•˜๊ธฐ๋งŒ ํ•œ๋‹ค๋ฉด, ์ ‘์ด‰๋ถ€(๋ณธ ์‹ค์‹œ์˜ˆ์—์„œ๋Š” ๋ฐ”ํ€ด 410a,410b์— ํ•ด๋‹น)์˜ ๊ตฌ์กฐ๋‚˜ ์ด๋™๋ถ€(400)์˜ ํ˜•์ƒ ๋“ฑ์ด ํŠน๋ณ„ํžˆ ์–ด๋Š ํ•œ๊ฐ€์ง€ ๊ตฌ์„ฑ์œผ๋กœ ์ œํ•œ์„ ๋ฐ›๋Š” ๊ฒƒ์€ ์•„๋‹ˆ๋‹ค. Such a structure may be viewed as a structure similar to the conventional ground displacement measuring apparatus described with reference to FIGS. 1 and 2. That is, the ground displacement measuring apparatus of the present embodiment is inserted into the inclined tube 500 excavated perpendicularly to the ground and is movable in the longitudinal direction (z direction), and only if the displacement of the inner surface of the inclined tube is detected by a contact type. (In this embodiment, the structure of the wheels 410a, 410b), the shape of the moving unit 400, etc. are not particularly limited to any one configuration.
์ด๋™๋ถ€(400) ๋‚ด์—๋Š” ์„ผ์‹ฑ์ˆ˜๋‹จ(110)์ด ์„ค์น˜๋œ ์„ผ์„œ๋ถ€(100)๊ฐ€ ๊ตฌ๋น„๋˜๋ฉฐ, ์„ผ์‹ฑ์ˆ˜๋‹จ(110)์€ ์ด๋™๋ถ€(400)๊ฐ€ ๊ฒฝ์‚ฌ๊ด€ ๋‚ด์—์„œ ๊ทธ ๊ธธ์ด๋ฐฉํ–ฅ์œผ๋กœ ์ด๋™์‹œ ํƒ€์ด๋ฐ์„ค์ •์ˆ˜๋‹จ(210)์— ์˜ํ•ด ์„ค์ •๋œ ์ธก์ • ํƒ€์ด๋ฐ๋งˆ๋‹ค 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„๋ฅผ ์‹ค์‹œ๊ฐ„์œผ๋กœ ์ธก์ •ํ•˜๊ฒŒ ๋œ๋‹ค. The moving part 400 is provided with a sensor part 100 provided with the sensing means 110, the sensing means 110 is the timing setting means 210 when the moving part 400 moves in the longitudinal direction in the inclined tube. Each 3D coordinate displacement is measured in real time.
์ด๋Ÿฌํ•œ ์„ผ์‹ฑ์ˆ˜๋‹จ(110)์œผ๋กœ์„œ ๋ฐ”๋žŒ์งํ•˜๊ฒŒ๋Š” MEMS(Micro Electro Mechanical System) ๊ธฐ์ˆ ๋กœ ๊ตฌํ˜„๋œ 3์ถ• ์Ÿˆ์ด๋กœ์„ผ์„œ ๋˜๋Š” 3์ถ• ๊ฐ€์†๋„์„ผ์„œ์™€ ๊ฐ™์€ ๊ด€์„ฑ์„ผ์„œ๊ฐ€ ์‚ฌ์šฉ๋œ๋‹ค. As the sensing means 110, an inertial sensor such as a three-axis gyro sensor or a three-axis acceleration sensor, which is preferably implemented by MEMS (Micro Electro Mechanical System) technology, is used.
์ตœ๊ทผ MEMS ๊ธฐ์ˆ ์˜ ๋ฐœ๋‹ฌ๋กœ ํฌ๊ธฐ๊ฐ€ ๋งค์šฐ ์ž‘๊ณ  ๊ฐ€๊ฒฉ๋„ ์ €๋ ดํ•œ ์Ÿˆ์ด๋กœ์„ผ์„œ(๊ฐ์†๋„ ์„ผ์„œ) ๋ฐ ๊ฐ€์†๋„์„ผ์„œ์˜ ๊ฐœ๋ฐœ์ด ํ™œ๋ฐœํ•˜๊ฒŒ ์ด๋ฃจ์–ด์ง€๊ณ  ์žˆ๋‹ค. ์ตœ๊ทผ ์ œํ’ˆํ™”๋œ ๊ฐ€์†๋„ ์„ผ์„œ๋Š” ์ฒด์ ์ด ์•ฝ ((2-3)mm)3์ •๋„ ์ดํ•˜์ด๋ฉฐ ๋งค๋…„ ๊ทธ ์ •๋ฐ€๋„๊ฐ€ ํ–ฅ์ƒ๋˜๋Š” ์ถ”์„ธ์ด๋‹ค. Recently, with the development of MEMS technology, development of gyro sensors (angular velocity sensors) and acceleration sensors, which are very small and inexpensive, is being actively conducted. Recently, accelerometers have a volume of about ((2-3) mm) 3 or less and their accuracy is increasing every year.
๋ณธ ์‹ค์‹œ์˜ˆ์˜ MEMS ์Ÿˆ์ด๋กœ์„ผ์„œ๋กœ์„œ๋Š”, ์˜ˆ๋ฅผ ๋“ค์–ด ์ฝ”๋ฆฌ์˜ฌ๋ฆฌ์˜ ํž˜์„ ์ด์šฉํ•˜๋Š” ๊ณต์ง€์˜ ์ง„๋™ํ˜• ์Ÿˆ์ด๋กœ์„ผ์„œ๊ฐ€ ์ ์šฉ๋  ์ˆ˜ ์žˆ์œผ๋ฉฐ, MEMS ๊ฐ€์†๋„์„ผ์„œ๋กœ์„œ๋Š”, ์˜ˆ๋ฅผ ๋“ค์–ด ์งˆ๋Ÿ‰์ฒด์™€ ๋ฐ”๋„ค ๋“ฑ์œผ๋กœ ๊ตฌ์„ฑ๋œ ๊ณต์ง€์˜ ์ •์ „์šฉ๋Ÿ‰ํ˜• ๊ฐ€์†๋„์„ผ์„œ ๋˜๋Š” ํ”ผ์—์กฐ(Piezo) ์ €ํ•ญ ๋ณ€ํ™”๋ฅผ ์ด์šฉํ•œ ๊ฐ€์†๋„์„ผ์„œ ๋“ฑ์ด ์ ์šฉ๋  ์ˆ˜ ์žˆ๋‹ค. As the MEMS gyro sensor of the present embodiment, for example, a known vibration type gyro sensor using the force of Coriolis can be applied. As the MEMS acceleration sensor, for example, a known capacitive acceleration sensor composed of a mass body and a banet or the like, or An acceleration sensor using a piezo resistance change may be applied.
๋ณธ ์‹ค์‹œ์˜ˆ์—์„œ๋Š” ์ด๋ ‡๊ฒŒ MEMS ๊ธฐ์ˆ ๋กœ ๊ตฌํ˜„๋œ 3์ถ• ์Ÿˆ์ด๋กœ์„ผ์„œ ๋˜๋Š” 3์ถ• ๊ฐ€์†๋„์„ผ์„œ๋ฅผ ์‚ฌ์šฉํ•จ์œผ๋กœ์จ, ์„ผ์„œ๋ถ€(100)์™€ ์ด๋™๋ถ€(400)์˜ ํฌ๊ธฐ๋ฅผ ์ตœ๋Œ€ํ•œ ์ž‘๊ฒŒ ๊ตฌํ˜„ํ•˜๋Š” ํšจ๊ณผ๋ฅผ ์ œ๊ณตํ•œ๋‹ค. In this embodiment, by using a three-axis gyro sensor or a three-axis acceleration sensor implemented by the MEMS technology, thereby providing the effect of implementing the size of the sensor unit 100 and the moving unit 400 as small as possible.
๊ธฐ๋ณธ์ ์œผ๋กœ ์–ด๋–ค ๋ฌผ์ฒด์˜ ์›€์ง์ž„๊ณผ ์ ˆ๋Œ€์ขŒํ‘œ์˜ ๋ณ€ํ™”๋ฅผ ๋…๋ฆฝ์ ์œผ๋กœ ์ธก์ •ํ•˜๋Š” ๊ฒƒ์€, 3์ถ•(x,y,z)์˜ ๊ฐ์†๋„ ๋˜๋Š” 3์ถ•์˜ ๊ฐ€์†๋„๋ฅผ ๊ฒ€์ถœํ•˜๊ณ  ์ด๋ฅผ ์ ๋ถ„์ฒ˜๋ฆฌ ํ•˜๋Š” ๋ฐฉ์‹์œผ๋กœ ๊ฐ€๋Šฅํ•˜๋‹ค. Basically, it is possible to independently measure the movement of an object and the change in absolute coordinates by detecting the angular velocity of three axes (x, y, z) or acceleration of three axes and integrating them.
์Ÿˆ์ด๋กœ์„ผ์„œ ๋˜๋Š” ๊ฐ€์†๋„์„ผ์„œ๋Š” ๋ชจ๋‘ ์›€์ง์ž„์„ ๊ฐ์ง€ํ•˜๊ธฐ ์œ„ํ•ด ๊ด€์„ฑ๋ ฅ์„ ์ด์šฉํ•˜๋Š” ์„ผ์„œ๋กœ์„œ, ์„ผ์„œ ๋‚ด์— ๊ตฌ๋น„๋œ ์งˆ๋Ÿ‰์— ์ž‘์šฉํ•˜๋Š” ๊ด€์„ฑ๋ ฅ์„ ์ „์ž๊ธฐ์ ์ธ ์›๋ฆฌ๋กœ ์ธก์ •ํ•˜๊ณ  ์ด๋ฅผ ํ†ตํ•ด ๊ฐ์†๋„ ๋˜๋Š” ๊ฐ€์†๋„๊ฐ’์„ ๊ตฌํ•˜๋Š” ์„ผ์„œ์ด๋‹ค. ์ด๋ ‡๊ฒŒ ๊ตฌํ•ด์ง„ ๊ฐ์†๋„ ๋˜๋Š” ๊ฐ€์†๋„๊ฐ’์— ๋Œ€ํ•ด ์šด๋™๋ฐฉ์ •์‹์„ ๊ณ ๋ คํ•œ ์ ๋ถ„์ฒ˜๋ฆฌ๋ฅผ ํ•˜๊ฒŒ ๋˜๋ฉด ์ด๋™์‹œ์˜ ์ขŒํ‘œ ๋ณ€์œ„๋ฅผ ๊ตฌํ•  ์ˆ˜ ์žˆ๊ฒŒ ๋œ๋‹ค. ์˜ˆ๋ฅผ ๋“ค์–ด, ๊ฐ€์†๋„๊ฐ’์„ 2๋ฒˆ ์ ๋ถ„์ฒ˜๋ฆฌํ•˜๋ฉด ์ขŒํ‘œ ๋ณ€์œ„๊ฐ’์ด ๊ตฌํ•ด์ง„๋‹ค.Gyro sensors or acceleration sensors are all sensors that use inertial force to detect movement. The gyro sensor or acceleration sensor measures the inertial force acting on the mass provided in the sensor based on the electromagnetic principle and obtains the angular velocity or acceleration value. Integrating the angular velocity or acceleration value in this way into consideration of the equations of motion results in obtaining the coordinate displacement during the movement. For example, the coordinate displacement value is obtained by integrating the acceleration value twice.
๋ณธ ์‹ค์‹œ์˜ˆ์— ๋”ฐ๋ฅด๋ฉด, ์ด๋™๋ถ€(400)๊ฐ€ ๊ฒฝ์‚ฌ๊ด€ ๋‚ด์—์„œ ๊ทธ ๊ธธ์ด๋ฐฉํ–ฅ์œผ๋กœ ์ด๋™์‹œ์— ํƒ€์ด๋ฐ์„ค์ •์ˆ˜๋‹จ(210)์— ์˜ํ•ด ์„ค์ •๋œ ์ธก์ • ํƒ€์ด๋ฐ๋งˆ๋‹ค ์„ผ์‹ฑ์ˆ˜๋‹จ(110)์ด ์œ„์™€ ๊ฐ™์€ ์›๋ฆฌ๋กœ์„œ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„๋ฅผ ์‹ค์‹œ๊ฐ„์œผ๋กœ ์ธก์ •ํ•˜๊ฒŒ ๋œ๋‹ค. According to the present embodiment, when the moving unit 400 moves in the longitudinal direction in the inclined tube, the sensing means 110 measures the three-dimensional coordinate displacement in real time for each measurement timing set by the timing setting means 210. Will be measured.
์ด๋Ÿฌํ•œ ์„ผ์‹ฑ์ˆ˜๋‹จ(110)์€ ๊ฐ€์†๋„์„ผ์„œ๋ฅผ ์˜ˆ๋กœ ๋“ค๋ฉด, 1์ถ• ๊ฐ€์†๋„์„ผ์„œ 3๊ฐœ๋ฅผ x,y,z ๊ฐ ๋ฐฉํ–ฅ์œผ๋กœ 90๋„ ๊ฐ„๊ฒฉ์œผ๋กœ ์กฐํ•ฉํ•˜์—ฌ ์„ค์น˜ํ•œ ๊ตฌ์กฐ์ผ ์ˆ˜๋„ ์žˆ๊ณ , 2์ถ• ๊ฐ€์†๋„์„ผ์„œ์™€ 1์ถ• ๊ฐ€์†๋„์„ผ์„œ์˜ ์กฐํ•ฉ ๊ตฌ์กฐ์ผ ์ˆ˜๋„ ์žˆ์œผ๋ฉฐ, ๋‹จ์ผ ํŒจํ‚ค์ง•ํ™”๋œ ํ•˜๋‚˜์˜ 3์ถ• ๊ฐ€์†๋„์„ผ์„œ์ผ ์ˆ˜๋„ ์žˆ๋‹ค. ์ฆ‰, 3์ถ•์˜ ๊ฐ์†๋„ ๋˜๋Š” ๊ฐ€์†๋„๋ฅผ ์ธก์ •ํ•  ์ˆ˜๋งŒ ์žˆ์œผ๋ฉด, ์„ผ์‹ฑ์ˆ˜๋‹จ(110)์˜ ๊ตฌ์กฐ๊ฐ€ ํŠน๋ณ„ํžˆ ์–ด๋Š ํ•œ๊ฐ€์ง€ ๊ตฌ์„ฑ์œผ๋กœ ์ œํ•œ์„ ๋ฐ›๋Š” ๊ฒƒ์€ ์•„๋‹ˆ๋‹ค. For example, the sensing means 110 may be a structure in which three single-axis acceleration sensors are installed by combining the three-axis acceleration sensors at 90-degree intervals in the x, y, and z directions, respectively, and the two-axis acceleration sensor and the single-axis acceleration sensor. It may be a combination structure of, or may be a single packaged three-axis acceleration sensor. That is, as long as the angular velocity or acceleration of the three axes can be measured, the structure of the sensing means 110 is not particularly limited to any one configuration.
๋˜ํ•œ, ์ธก์ • ์‹ ํ˜ธ ์ฒ˜๋ฆฌ์— ์žˆ์–ด์„œ ํ†ต์ƒ์ ์œผ๋กœ ์‚ฌ์šฉ๋˜๋Š” ์ฆํญํšŒ๋กœ ๋ฐ AD ์ปจ๋ฒ„ํ„ฐ(converter)๊ฐ€ ์„ผ์„œ๋ถ€(100) ๋‚ด์— ๊ตฌ๋น„๋  ์ˆ˜ ์žˆ์ง€๋งŒ, ๋ณ„๋„๋กœ ๋„๋ฉด์— ๋„์‹œํ•˜์ง€๋Š” ์•Š์•˜๋‹ค. ์ฆํญํšŒ๋กœ ๋ฐ AD ์ปจ๋ฒ„ํ„ฐ(converter)๋Š” ๊ฐ๊ฐ์˜ ์œ ๋‹›์œผ๋กœ ์„ผ์„œ๋ถ€(100) ๋‚ด์— ์„ค์น˜๋  ์ˆ˜๋„ ์žˆ์œผ๋ฉฐ, ์ตœ๊ทผ์˜ ์„ผ์„œ ๋ชจ๋“ˆํ™” ๊ฒฝํ–ฅ์— ๋”ฐ๋ผ ์Ÿˆ์ด๋กœ์„ผ์„œ ๋˜๋Š” ๊ฐ€์†๋„์„ผ์„œ ๋ชจ๋“ˆ ๋‚ด์— ์ผ์ฒดํ™”๋œ ํ˜•ํƒœ๋กœ ๊ตฌ๋น„๋  ์ˆ˜๋„ ์žˆ๋‹ค.In addition, an amplifier circuit and an AD converter which are commonly used in measuring signal processing may be provided in the sensor unit 100, but are not separately illustrated in the drawings. The amplifying circuit and the AD converter may be installed in the sensor unit 100 as each unit, or may be provided in an integrated form in a gyro sensor or an acceleration sensor module according to the recent sensor module trend.
์ด๋ ‡๊ฒŒ ์„ผ์‹ฑ์ˆ˜๋‹จ(110)์—์„œ ์ธก์ •ํ•œ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„ ๋ฐ์ดํ„ฐ๋Š” ์ „์„ (๋˜๋Š” ์‹ ํ˜ธ์„ , 300)์„ ํ†ตํ•ด ์ง€์ƒ์— ์œ„์น˜ํ•œ ์—ฐ์‚ฐ์ œ์–ด๋ถ€(200)๋กœ ์ „์†ก๋˜๋ฉฐ, ์—ฐ์‚ฐ์ œ์–ด๋ถ€(200) ๋‚ด์— ๊ตฌ๋น„๋œ ๋ณ€์œ„๋Ÿ‰์—ฐ์‚ฐ์ˆ˜๋‹จ(220)์— ์˜ํ•ด ์ง€๋ฐ˜๋ณ€์œ„๋Ÿ‰์œผ๋กœ ์—ฐ์‚ฐ๋˜์–ด ์ž‘์—…์ž์—๊ฒŒ ๋””์Šคํ”Œ๋ ˆ์ด ๋œ๋‹ค. ์ด๋ฅผ ํ†ตํ•ด ์ž‘์—…์ž๋Š” ์ง€๋ฐ˜์ด์™„ ๋˜๋Š” ๊ทธ ๋ณ€์œ„์˜ ์œ„์น˜์™€ ๋ฐฉํ–ฅ, ํฌ๊ธฐ ๋“ฑ์„ ํŒŒ์•…ํ•  ์ˆ˜ ์žˆ๊ฒŒ ๋œ๋‹ค. ์ด๋Ÿฌํ•œ ์ „์ฒด ๊ณผ์ •์€ ๋„ 6์˜ S520 ๋‚ด์ง€ S560 ๋‹จ๊ณ„๋กœ ์ด๋ค„์ง„ ์ž‘๋™ํ๋ฆ„๋„๋ฅผ ํ†ตํ•ด ๋ณด๋‹ค ์ƒ์„ธํ•˜๊ฒŒ ์ดํ•ด๋  ์ˆ˜ ์žˆ๋‹ค. The three-dimensional coordinate displacement data measured by the sensing means 110 is transmitted to the calculation control unit 200 located on the ground through the wire (or signal line, 300), displacement calculation unit 220 provided in the calculation control unit 200 It is calculated by ground displacement and displayed to the operator. Through this, the worker can grasp the position, direction, and size of the ground relaxation or its displacement. This entire process can be understood in more detail through the operation flow chart consisting of the steps S520 to S560 of FIG.
๋ณด๋‹ค ์ƒ์„ธํ•˜๊ฒŒ, ์Ÿˆ์ด๋กœ์„ผ์„œ ๋˜๋Š” ๊ฐ€์†๋„์„ผ์„œ๊ฐ€ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„๋ฅผ ์ธก์ •ํ•˜๋Š” ๊ณผ์ •์€ ๋‹ค์Œ๊ณผ ๊ฐ™์ด ์ดํ•ด๋  ์ˆ˜ ์žˆ๋‹ค. More specifically, the process of measuring the three-dimensional coordinate displacement by the gyro sensor or the acceleration sensor can be understood as follows.
๊ฒฝ์‚ฌ๊ด€(500) ๋‚ด์—์„œ ์ด๋™๋ถ€(400)์˜ ์ถœ๋ฐœ ์ง€์ ์„ ๊ธฐ์ค€์ ์œผ๋กœ ์„ค์ •ํ•˜๊ณ  ์ด๋™๋ถ€(400)๋ฅผ ์Šน๊ฐ•(๋˜๋Š” ํ•˜๊ฐ•)ํ•˜๊ฒŒ ๋˜๋ฉด, ์„ค์ •๋œ ์ฃผํŒŒ์ˆ˜ ์‹œ์ ๋งˆ๋‹ค ์Ÿˆ์ด๋กœ์„ผ์„œ ๋˜๋Š” ๊ฐ€์†๋„์„ผ์„œ๊ฐ€ ๋ฐ”๋กœ ์ง์ „ ์ธก์ • ์‹œ์ ์—์„œ์˜ ์ด๋™๋ถ€ ์œ„์น˜๋ฅผ ๊ธฐ์ค€์œผ๋กœ ํ˜„ ์ธก์ • ์‹œ์ ์˜ ์ด๋™๋ถ€์˜ ์ƒ๋Œ€ ์œ„์น˜๋ฅผ ์ธก์ •ํ•œ๋‹ค. ์ด๋Ÿฌํ•œ ๋ฐฉ์‹์œผ๋กœ, ์ตœ์ดˆ ์ถœ๋ฐœ ์ง€์ ์ธ ๊ธฐ์ค€์ ์— ๋Œ€ํ•œ ์ด๋™๋ถ€(400)์˜ ์—ฐ์†์ ์ธ ์ƒ๋Œ€ ๋ณ€์œ„๋ฅผ ๊ตฌํ•˜๋ฉด, ์ตœ์ดˆ ๊ธฐ์ค€์  ์œ„์น˜๋ฅผ ์ค‘์‹ฌ์œผ๋กœ ๊ฒฝ์‚ฌ๊ด€ ๋‚ด๋ฉด์˜ ์ „์ฒด 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„๊ฐ€ ๊ตฌํ•ด์ง€๊ฒŒ ๋œ๋‹ค. ์ด๋•Œ, ์ด๋™๋ถ€(400)์˜ ์ด๋™์†๋„๋Š” ๊ณ ์ • ์†๋„์ธ ๊ฒƒ์ด ๋ฐ”๋žŒ์งํ•˜์ง€๋งŒ, ์ด๋™ ์ค‘์— ์†๋„๊ฐ€ ๋ฐ”๋€Œ์–ด๋„ ๋ฌธ์ œ๋Š” ์—†๋‹ค. When the starting point of the moving unit 400 is set as the reference point in the inclined tube 500 and the moving unit 400 is moved up (or lowered), the gyro sensor or the acceleration sensor is measured at the immediately preceding measurement point at each set frequency point. The relative position of the moving unit at the current measurement time is measured based on the position of the moving unit. In this way, when the continuous relative displacement of the moving unit 400 with respect to the reference point, which is the first starting point, is obtained, the total three-dimensional coordinate displacement of the inner surface of the inclined tube is obtained based on the position of the first reference point. At this time, the moving speed of the moving unit 400 is preferably a fixed speed, but there is no problem even if the speed changes during the movement.
3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„ ์—ฐ์‚ฐ์€ ์„ผ์„œ๋ถ€(100) ๋‚ด์—์„œ ์ง์ ‘ ์ด๋ค„์งˆ ์ˆ˜๋„ ์žˆ์œผ๋ฉฐ, ์ง€์ƒ์˜ ์—ฐ์‚ฐ์ œ์–ด๋ถ€(200)์—์„œ ์ด๋ค„์งˆ ์ˆ˜๋„ ์žˆ๋‹ค. The three-dimensional coordinate displacement calculation may be performed directly in the sensor unit 100, or may be performed in the ground operation control unit 200.
์ฆ‰, ์ด๋™๋ถ€(400)๋‚ด์— ์„ค์น˜๋˜๋Š” ์„ผ์„œ๋ถ€(100)๋ฅผ SoC(System on Chip) ํ˜•ํƒœ๋กœ ์ œ์ž‘ํ•˜๊ณ  3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„ ์—ฐ์‚ฐ ๋ชจ๋“ˆ์„ SoC(System on Chip) ๋‚ด์— ํ•˜๋‚˜์˜ ์นฉ ํ˜•ํƒœ๋กœ ์ œ์ž‘ํ•˜๋Š” ๋ฐฉ์‹๋„ ๊ฐ€๋Šฅํ•˜๊ณ , ์„ผ์„œ๋ถ€(100)์—๋Š” ์Ÿˆ์ด๋กœ์„ผ์„œ(๋˜๋Š” ๊ฐ€์†๋„์„ผ์„œ)์™€ ์ฆํญํšŒ๋กœ, AD ์ปจ๋ฒ„ํ„ฐ๋งŒ ์„ค์น˜ํ•˜๊ณ  3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„ ์—ฐ์‚ฐ์€ ์ง€์ƒ์˜ ์—ฐ์‚ฐ์ œ์–ด๋ถ€(200)์—์„œ ์ด๋ค„์ง€๋„๋ก ๊ตฌ์„ฑํ•˜๋Š” ๊ฒƒ๋„ ๊ฐ€๋Šฅํ•˜๋‹ค. In other words, the sensor unit 100 installed in the moving unit 400 may be manufactured in the form of a system on chip (SoC), and the three-dimensional coordinate displacement module may be manufactured in the form of a single chip in the system on chip (SoC). In addition, only the gyro sensor (or the acceleration sensor), the amplification circuit, and the AD converter are installed in the sensor unit 100, and the three-dimensional coordinate displacement calculation may be configured to be performed by the ground operation control unit 200.
์—ฐ์‚ฐ์ œ์–ด๋ถ€(200)์—๋Š” ์ „์›(230) ๋ฐ ๋””์Šคํ”Œ๋ ˆ์ด๋ถ€(๋„๋ฉด ๋ฏธ๋„์‹œ) ๋“ฑ์ด ๊ตฌ๋น„๋˜๋ฉฐ, ํ†ต์ƒ์ ์ธ ๊ณ„์ธก์žฅ์น˜์— ๊ตฌ๋น„๋˜๋Š” ๋ถ€๊ฐ€์  ๊ธฐ๋Šฅ์š”์†Œ๊ฐ€ ์ถ”๊ฐ€์ ์œผ๋กœ ๊ตฌ๋น„๋  ์ˆ˜ ์žˆ๋‹ค. The operation control unit 200 is provided with a power supply 230 and a display unit (not shown), and may be additionally provided with additional functional elements included in a conventional measuring device.
๋˜ํ•œ, ํƒ€์ด๋ฐ ์„ค์ •์ˆ˜๋‹จ(210)์€ ์—ฐ์‚ฐ์ œ์–ด๋ถ€(200) ๋‚ด์— ์„ค์น˜๋˜๋Š” ๊ฒƒ์œผ๋กœ ์˜ˆ์‹œ๋˜์—ˆ์ง€๋งŒ, ํ•„์š”์— ๋”ฐ๋ผ ์„ผ์„œ๋ถ€(100) ๋‚ด์— ์„ค์น˜๋  ์ˆ˜ ์žˆ์Œ์€ ๋ฌผ๋ก ์ด๋‹ค. In addition, although the timing setting unit 210 is illustrated as being installed in the operation control unit 200, it may be installed in the sensor unit 100 as necessary.
ํƒ€์ด๋ฐ์„ค์ •์ˆ˜๋‹จ(210)์„ ํ†ตํ•ด ์„ค์ •๋˜๋Š” ์ธก์ • ํƒ€์ด๋ฐ์€, ์„ผ์‹ฑ์ˆ˜๋‹จ(110)์ด ์„ผ์‹ฑ ๋™์ž‘์„ ์ˆ˜ํ–‰ํ•˜๋Š” ์ธก์ • ์‹œ๊ฐ„ ๊ฐ„๊ฒฉ์„ ์˜๋ฏธํ•˜๋ฉฐ, ์ฃผํŒŒ์ˆ˜ ๊ฐœ๋…์œผ๋กœ ์ดํ•ด๋  ์ˆ˜ ์žˆ๋‹ค. The measurement timing set through the timing setting means 210 means a measurement time interval in which the sensing means 110 performs a sensing operation, and can be understood as a frequency concept.
์˜ˆ๋ฅผ ๋“ค์–ด, ์ธก์ • ํƒ€์ด๋ฐ์„ ์ฃผํŒŒ์ˆ˜ ๊ฐœ๋…์œผ๋กœ 25Hz๋กœ ์„ค์ •ํ•˜๊ฒŒ ๋˜๋ฉด, 1์ดˆ๋‹น ์„ผ์‹ฑ์ˆ˜๋‹จ(110)์ด 25๋ฒˆ์˜ ์„ผ์‹ฑ ๋™์ž‘์„ ์ˆ˜ํ–‰ํ•˜๊ฒŒ ๋˜๋ฉฐ, ์ด๋™๋ถ€(400)์˜ ์ด๋™ ์ค‘์— ์ด๋Ÿฌํ•œ ์„ผ์‹ฑ ๋™์ž‘์ด ์ด๋ค„์ง„๋‹ค๋Š” ๊ฒƒ์€ ๊ฒฐ๊ตญ 1์ดˆ๋‹น 25๋ฒˆ์˜ ์ขŒํ‘œ ๋ณ€์œ„ ์ธก์ •์ด ์ด๋ค„์ง„๋‹ค๋Š” ๊ฒƒ์„ ์˜๋ฏธํ•œ๋‹ค. For example, when the measurement timing is set to 25 Hz as the frequency concept, the sensing means 110 performs 25 sensing operations per second, and the sensing operation is performed during the movement of the moving unit 400. This means that 25 coordinate displacement measurements are made per second.
์ด๋ ‡๊ฒŒ ์ฃผํŒŒ์ˆ˜ ๋ฐฉ์‹์œผ๋กœ ์ขŒํ‘œ ๋ณ€์œ„ ์ธก์ •์„ ํ•˜๊ฒŒ ๋˜๋ฏ€๋กœ, ๋ณธ ๋ฐœ๋ช…์— ๋”ฐ๋ฅธ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜๋Š” ์ข…๋ž˜์™€ ๋‹ฌ๋ฆฌ ์ตœ์†Œ ์ธก์ • ๊ฐ„๊ฒฉ์ด๋‚˜ ๊ธฐ์ค€์  ๋“ฑ์„ ๊ณ ๋ คํ•  ํ•„์š” ์—†์ด ์ธก์ • ๊ณผ์ •์ด ์‹ค์‹œ๊ฐ„์œผ๋กœ ์—ฐ์†์ ์œผ๋กœ ์ด๋ค„์ง€๊ฒŒ ๋˜์–ด, ๊ธฐ์ค€์ ์˜ ๋ถˆ์ผ์น˜ ๋˜๋Š” ์ฒœ๊ณต์ˆ˜์ง๋„, ๊ฒฝ์‚ฌ๊ด€ ๋น„ํ‹€๋ฆผ ๋“ฑ์œผ๋กœ ๋ฐœ์ƒํ–ˆ๋˜ ์ข…๋ž˜์˜ ์ธก์ •์˜ค์ฐจ ๋ฌธ์ œ๋ฅผ ํ•ด๊ฒฐํ•ด ์ค€๋‹ค. Since the coordinate displacement measurement is performed in such a manner, the ground displacement measuring apparatus according to the present invention does not have to consider a minimum measurement interval or a reference point, unlike the conventional method, and the measurement process is continuously performed in real time. This solves the problem of conventional measurement errors caused by torsional torsion.
๋˜ํ•œ, MEMS ๊ธฐ์ˆ ๋กœ ๊ตฌํ˜„๋œ ์†Œํ˜• ์„ผ์„œ๋ฅผ ์‚ฌ์šฉํ•˜์—ฌ ์ด๋™๋ถ€(400)์˜ ๊ธธ์ด๋ฅผ ์ข…๋ž˜์— ๋น„ํ•ด ์ž‘๊ฒŒ ์ œ์ž‘ํ•  ์ˆ˜ ์žˆ์œผ๋ฏ€๋กœ, ์ด๋™๋ถ€(400)์˜ ์ƒํ•˜ ๋ฐ”ํ€ด(410a,410b) ๊ฐ„๊ฒฉ ์ดํ•˜์˜ ๊ณก๋ฅ ๋ฐ˜๊ฒฝ์„ ์ง€๋‹ˆ๋Š” ๊ธ‰๊ฒฉํ•˜๊ณ  ๋ฏธ์„ธํ•œ ๊ฒฝ์‚ฌ๋„ ์ •๋ฐ€ํ•˜๊ฒŒ ์ธก์ •ํ•  ์ˆ˜ ์žˆ์œผ๋ฉฐ, ๊ธ‰๊ฒฉํ•œ ๊ฒฝ์‚ฌ์—๋„ ์ด๋™๋ถ€์˜ ํˆฌ์ž…์ด ๊ฐ€๋Šฅํ•œ ์žฅ์ ์„ ์ œ๊ณตํ•œ๋‹ค. In addition, since the length of the moving part 400 can be made smaller than the conventional method using a small sensor implemented by MEMS technology, the moving part 400 has a radius of curvature of less than or equal to the interval between the upper and lower wheels 410a and 410b. The fine inclination can be measured precisely, and it provides the advantage that the moving part can be inserted even in the steep inclination.
ํ•œํŽธ, ๋ณธ ์‹ค์‹œ์˜ˆ์—์„œ๋Š” MEMS ๊ธฐ์ˆ ๋กœ ๊ตฌํ˜„๋œ 3์ถ• ์Ÿˆ์ด๋กœ์„ผ์„œ ๋˜๋Š” 3์ถ• ๊ฐ€์†๋„์„ผ์„œ๋ฅผ ์˜ˆ์‹œํ•˜์ง€๋งŒ, ์ด๋™๋ถ€์˜ ์ด๋™ ๊ณผ์ • ์ค‘์— ์ธก์ • ํƒ€์ด๋ฐ์— ๋งž์ถฐ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„์— ๋Œ€ํ•œ ์„ผ์‹ฑ ๋™์ž‘์„ ์ˆ˜ํ–‰ํ•  ์ˆ˜ ์žˆ๋Š” ์„ผ์‹ฑ์ˆ˜๋‹จ์ด๋ผ๋ฉด, ์˜ˆ์‹œ๋œ ๊ฒƒ์— ํ•œ์ •๋˜์ง€ ์•Š๊ณ  ๋ณธ ๋ฐœ๋ช…์˜ ๋ฒ”์ฃผ์— ํฌํ•จ๋จ์ด ๋‹น์—ฐํ•˜๋‹ค. ํŠนํžˆ, ์†Œํ˜•์˜ ํฌ๊ธฐ๋ฅผ ๊ฐ€์ง„ ๊ฒƒ์ด๋ผ๋ฉด ๋ฐ”๋žŒ์งํ•˜๊ฒŒ ์ ์šฉ๋  ์ˆ˜ ์žˆ๋‹ค. On the other hand, the present embodiment illustrates a three-axis gyro sensor or three-axis acceleration sensor implemented by MEMS technology, but if the sensing means that can perform the sensing operation for the three-dimensional coordinate displacement in accordance with the measurement timing during the movement of the moving part Naturally, the present invention is not limited to the illustrated ones, but is included in the scope of the present invention. In particular, it can be preferably applied if it has a small size.
๋„ 7์€ ๋ณธ ๋ฐœ๋ช…์˜ ๋˜๋‹ค๋ฅธ ์‹ค์‹œ์˜ˆ์— ์˜ํ•œ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜์˜ ์ž‘๋™ํ๋ฆ„๋„์ด๋‹ค. 7 is an operation flowchart of the ground displacement measuring apparatus according to another embodiment of the present invention.
๋ณธ ์‹ค์‹œ์˜ˆ์—์„œ, ์„ผ์‹ฑ์ˆ˜๋‹จ์€ 2์ถ• ์Ÿˆ์ด๋กœ์„ผ์„œ ๋˜๋Š” 2์ถ• ๊ฐ€์†๋„์„ผ์„œ ์ค‘์˜ ์–ด๋Š ํ•˜๋‚˜์™€ ์ง€๋ฐ˜ ์ˆ˜์ง๋ฐฉํ–ฅ ์ด๋™๊ฑฐ๋ฆฌ ์ธก์ •์„ผ์„œ์˜ ์กฐํ•ฉ์œผ๋กœ ์ด๋ค„์ง„๋‹ค. In this embodiment, the sensing means comprises a combination of either a two-axis gyro sensor or a two-axis acceleration sensor and a ground vertical movement distance measuring sensor.
์•ž์˜ ์‹ค์‹œ์˜ˆ์—์„œ๋Š” 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„๋ฅผ ์ธก์ •ํ•˜๊ธฐ ์œ„ํ•˜์—ฌ 3์ถ• ์Ÿˆ์ด๋กœ์„ผ์„œ ๋˜๋Š” 3์ถ• ๊ฐ€์†๋„์„ผ์„œ๋ฅผ ์‚ฌ์šฉํ•˜์ง€๋งŒ, ๋ณธ ์‹ค์‹œ์˜ˆ์—์„œ๋Š” x, y 2์ถ• ๋ฐฉํ–ฅ์˜ ์„ผ์‹ฑ์„ ํ•˜๋Š” 2์ถ• ์Ÿˆ์ด๋กœ์„ผ์„œ ๋˜๋Š” 2์ถ• ๊ฐ€์†๋„์„ผ์„œ์™€ ์ง€๋ฐ˜ ์ˆ˜์ง๋ฐฉํ–ฅ(z ๋ฐฉํ–ฅ) ์ด๋™๊ฑฐ๋ฆฌ ์ธก์ •์„ผ์„œ๋ฅผ ์กฐํ•ฉํ•˜์—ฌ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„๋ฅผ ์ธก์ •ํ•œ๋‹ค. In the previous embodiment, a three-axis gyroscope or a three-axis acceleration sensor is used to measure the three-dimensional coordinate displacement, but in this embodiment, a two-axis gyroscope or two-axis acceleration sensing in the x- and y-axis directions The three-dimensional coordinate displacement is measured by combining the sensor and the vertical distance (z direction) moving distance measuring sensor.
x, y 2์ถ•๊ณผ ๋‹ฌ๋ฆฌ, z ์ถ•์€ ์ด๋™๋ถ€(400)๊ฐ€ ๊ฒฝ์‚ฌ๊ด€์„ ๋”ฐ๋ผ ์ด๋™ํ•˜๋Š” ๋ฐฉํ–ฅ์ด๋ฏ€๋กœ, ์ด๋™ ๊ฒฝ๋กœ ์ค‘์— ๋ฌผ๋ฆฌ์  ์žฅ์•  ์š”์ธ์ด ๋ฐœ์ƒํ•œ ๊ฒฝ์šฐ๋ฅผ ๊ณ ๋ คํ•  ๋•Œ ์ด๋™๋Ÿ‰์„ ์ง์ ‘ ์ธก์ •ํ•˜๋Š” ์ง€๋ฐ˜ ์ˆ˜์ง๋ฐฉํ–ฅ(z ๋ฐฉํ–ฅ) ์ด๋™๊ฑฐ๋ฆฌ ์ธก์ •์„ผ์„œ๋ฅผ ์‚ฌ์šฉํ•˜๋Š” ๊ฒƒ์ด ๊ฐ€์†๋„ ๋“ฑ์˜ ๊ด€์„ฑ ๋ฌผ๋ฆฌ๋Ÿ‰์„ ์ธก์ •ํ•˜์—ฌ ๋ณ€์œ„๋ฅผ ์—ฐ์‚ฐํ•˜๋Š” ๋ฐฉ์‹๋ณด๋‹ค ์ธก์ • ์‹ ๋ขฐ๋„ ๋ฉด์—์„œ ์–‘ํ˜ธํ•  ์ˆ˜ ์žˆ๋‹ค. Unlike the x and y two axes, the z axis is a direction in which the moving part 400 moves along the inclined tube, so that the ground vertical direction (z direction) movement that directly measures the moving amount is considered when a physical obstacle occurs in the moving path. Using a distance sensor may be better in terms of measurement reliability than a method of calculating displacement by measuring an inertia physical quantity such as acceleration.
์ง€๋ฐ˜ ์ˆ˜์ง๋ฐฉํ–ฅ(z๋ฐฉํ–ฅ) ์ด๋™๊ฑฐ๋ฆฌ ์ธก์ •์„ผ์„œ๋Š” ์ „์„ (300)์˜ ์ด์†ก๋Ÿ‰์„ ํ†ตํ•ด ์ด๋™๋ถ€(400)์˜ ์ด๋™๋Ÿ‰์„ ์ธก์ •ํ•˜๋Š” ๊ณต์ง€์˜ ์„ผ์‹ฑ์ˆ˜๋‹จ์ด ์‚ฌ์šฉ๋  ์ˆ˜ ์žˆ์œผ๋ฉฐ, ์˜ˆ๋ฅผ ๋“ค์–ด, ๋‹ค์Œ๊ณผ ๊ฐ™์€ ๋ฐฉ์‹์œผ๋กœ ์ง€๋ฐ˜ ์ˆ˜์ง๋ฐฉํ–ฅ์„ ์ธก์ •ํ•œ๋‹ค. Ground vertical direction (z direction) movement distance measuring sensor may be a known sensing means for measuring the movement amount of the moving unit 400 through the transfer amount of the wire 300, for example, the ground vertical in the following manner Measure the direction.
๋„ 5๋ฅผ ์ฐธ์กฐํ•˜๋ฉด, ์ด๋™๋ถ€(400)์™€ ์—ฐ๊ฒฐ๋œ ์ „์„ (300)์— ์ง€๋ฐ˜์˜ ์ผ์ง€์ ์— ๊ณ ์ • ์„ค์น˜๋œ ์ธก์ •์šฉ ๋ฐ”ํ€ด๋ฅผ ์ ‘์ด‰์‹œํ‚ค๊ฒŒ ๋˜๋ฉด, ์ „์„ (300)์˜ ์ด๋™ ์‹œ ์ธก์ •์šฉ ๋ฐ”ํ€ด๋Š” ์ „์„ (300)๊ณผ์˜ ์ ‘์ด‰๋ ฅ์— ์˜ํ•ด ํšŒ์ „ํ•˜๊ฒŒ ๋œ๋‹ค. Referring to FIG. 5, when the measuring wheels are fixed to one point of the ground in contact with the wire 300 connected to the moving unit 400, the measuring wheels move with the wire 300 when the wire 300 is moved. It is rotated by the contact force.
์ด๋•Œ, ์ „์„ (300)์— ์˜ํ•œ ๋ฐ”ํ€ด ํšŒ์ „๋Ÿ‰์„ ์ธก์ •ํ•˜์—ฌ ์ด๋ฅผ ์ „์„ (300)์˜ ์ด๋™ ๊ฑฐ๋ฆฌ๋กœ ํ™˜์‚ฐํ•˜๊ฒŒ ๋˜๋ฉด, ์ „์„ (300)์— ์—ฐ๊ฒฐ๋œ ์ด๋™๋ถ€(400)์˜ z๋ฐฉํ–ฅ ์ด๋™๊ฑฐ๋ฆฌ์˜ ์ ˆ๋Œ€๊ฐ’์„ ๋น„๊ต์  ๊ฐ„๋‹จํ•˜๊ฒŒ ์ธก์ •ํ•  ์ˆ˜ ์žˆ๋‹ค. ์ธก์ •์šฉ ๋ฐ”ํ€ด๋Š” ๋„ 5์— ๋„์‹œ๋œ ์ „์„ (300) ์ง€์ง€์šฉ ๋กค๋Ÿฌ(420)๋ฅผ ๊ฒธ์šฉํ•˜์—ฌ ์‚ฌ์šฉํ•ด๋„ ๋˜๋ฉฐ, ์ „์„ (300)์— ์ ‘์ด‰ ๊ฐ€๋Šฅํ•œ ์–ด๋–ค ์œ„์น˜์— ์„ค์น˜๋  ์ˆ˜ ์žˆ๋‹ค. ๋˜ํ•œ, ์ ‘์ด‰์‹ ๋˜๋Š” ๋น„์ ‘์ด‰์‹ ์—ฌ๋ถ€์— ๊ด€๊ณ„์—†์ด ์ „์„ (300)์˜ ์ด๋™ ๊ฑฐ๋ฆฌ๋ฅผ ์ธก์ •ํ•  ์ˆ˜ ์žˆ๋Š” ์„ผ์‹ฑ ์ˆ˜๋‹จ์ด๋ผ๋ฉด ๊ณต์ง€๋œ ์–ด๋– ํ•œ ๋ฐฉ์‹์˜ ๊ฒƒ์ด ์‚ฌ์šฉ๋  ์ˆ˜ ์žˆ์Œ์€ ๋ฌผ๋ก ์ด๋‹ค. In this case, when the amount of wheel rotation by the wire 300 is measured and converted into the moving distance of the wire 300, the absolute value of the moving distance in the z-direction of the moving part 400 connected to the wire 300 is relatively simple. It can be measured. The measuring wheel may be used in combination with the support roller 420 of the wire 300 shown in FIG. 5, and may be installed at any position in contact with the wire 300. In addition, any sensing method capable of measuring the moving distance of the wire 300 regardless of whether it is contact or non-contact may be used in any known manner.
๋„ 1 ๋‚ด์ง€ ๋„ 2์— ์˜ˆ์‹œ๋œ ์ข…๋ž˜์˜ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜๋Š” ์ธก์ • ๊ฐ„๊ฒฉ์œผ๋กœ ๊ฐ€๋‹ค ์„œ๋‹ค๋ฅผ ๋ฐ˜๋ณตํ•˜๋Š” ๋ฐฉ์‹์ด๋ฏ€๋กœ, z๋ฐฉํ–ฅ์˜ ์˜ค์ฐจ๊ฐ€ ํ•„์—ฐ์ ์œผ๋กœ ๋ฐœ์ƒํ•˜๊ฒŒ ๋˜์–ด z๋ฐฉํ–ฅ ์ด๋™๊ฑฐ๋ฆฌ๋ฅผ ์ธ์‹ํ•˜์—ฌ ์ œ์–ดํ•˜๋Š” ๊ณผ์ •์ด ๋ณต์žกํ•  ์ˆ˜ ๋ฐ–์— ์—†์—ˆ๋‹ค. ๊ทธ๋Ÿฌ๋‚˜, ๋ณธ ์‹ค์‹œ์˜ˆ์— ์˜ํ•œ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜๋Š” ์ผ์ • ์†๋„๋กœ ์ด๋™๋ถ€(400)๋ฅผ ์Šนํ•˜๊ฐ•์‹œํ‚ค๋Š” ๋ฐฉ์‹์ด๋ฏ€๋กœ, ๊ฐ„๋‹จํ•œ ์•Œ๊ณ ๋ฆฌ์ฆ˜์„ ํ†ตํ•ด์„œ๋„ z๋ฐฉํ–ฅ์˜ ์œ„์น˜ ๋ฐ ์ด๋™๊ฑฐ๋ฆฌ๋ฅผ ์ •ํ™•ํ•˜๊ฒŒ ์ธก์ •ํ•  ์ˆ˜ ์žˆ๋‹ค. The conventional ground displacement measuring apparatus illustrated in FIGS. 1 and 2 repeats the stand-by-going measurement intervals, so that an error in the z direction is inevitably generated, and thus, a process of recognizing and controlling the moving distance in the z direction may be complicated. There was only. However, since the ground displacement measuring apparatus according to the present embodiment is a method of raising and lowering the moving unit 400 at a constant speed, the position and moving distance in the z direction can be accurately measured even through a simple algorithm.
์ƒ๊ธฐ ๊ตฌ์„ฑ์— ๋”ฐ๋ฅธ ์ธก์ • ๊ณผ์ •์€ ๋„ 7์˜ S522 ๋‚ด์ง€ S562 ๋‹จ๊ณ„๋กœ ์ด๋ค„์ง„ ์ž‘๋™ํ๋ฆ„๋„๋ฅผ ํ†ตํ•ด ๋ณด๋‹ค ์ƒ์„ธํ•˜๊ฒŒ ์ดํ•ด๋  ์ˆ˜ ์žˆ๋‹ค. The measurement process according to the above configuration can be understood in more detail through the operation flow chart made of the steps S522 to S562 of FIG.
๋„๋ฉด์„ ์ฐธ์กฐํ•˜์—ฌ ๋ณธ ๋ฐœ๋ช…์˜ ๋˜๋‹ค๋ฅธ ์‹ค์‹œ์˜ˆ์— ๋Œ€ํ•˜์—ฌ ์„ค๋ช…ํ•œ๋‹ค. Another embodiment of the present invention will be described with reference to the drawings.
๋„ 8์€ ๋ณธ ๋ฐœ๋ช…์˜ ๋˜๋‹ค๋ฅธ ์‹ค์‹œ์˜ˆ์— ์˜ํ•œ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜์˜ ๊ตฌ์„ฑ๋„, ๋„ 9๋Š” ๋ณธ ๋ฐœ๋ช…์˜ ๋˜๋‹ค๋ฅธ ์‹ค์‹œ์˜ˆ์— ์˜ํ•œ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜์˜ ์ž‘๋™ํ๋ฆ„๋„์ด๋‹ค.8 is a block diagram of a ground displacement measuring apparatus according to another embodiment of the present invention, Figure 9 is a flow chart of the ground displacement measuring apparatus according to another embodiment of the present invention.
๋ณธ ์‹ค์‹œ์˜ˆ์˜ ์„ผ์‹ฑ์ˆ˜๋‹จ์€ ์ƒํ˜ธ ๋…๋ฆฝ์ ์ธ ์ธก์ •๋ฐฉ์‹์„ ๊ฐ–๋Š” ๋ณต์ˆ˜์˜ ์„ผ์‹ฑ์ˆ˜๋‹จ(112,114)์œผ๋กœ ๊ตฌ์„ฑ๋œ๋‹ค. ๋…๋ฆฝ์ ์ธ ์ธก์ •๋ฐฉ์‹์ด๋ž€ ๊ฐ ์„ผ์‹ฑ์ˆ˜๋‹จ์ด ์„œ๋กœ ๋‹ค๋ฅธ ๋ฌผ๋ฆฌ์  ์ธก์ •์›๋ฆฌ๋ฅผ ์‚ฌ์šฉํ•œ๋‹ค๋Š” ์˜๋ฏธ๋กœ์„œ, ์˜ˆ๋ฅผ ๋“ค์–ด ๋ณต์ˆ˜์˜ ์„ผ์‹ฑ์ˆ˜๋‹จ์€ 3์ถ• ์Ÿˆ์ด๋กœ์„ผ์„œ์™€ 3์ถ• ๊ฐ€์†๋„์„ผ์„œ์˜ 2๊ฐœ์˜ ์„ผ์„œ๋กœ ๊ตฌ์„ฑ๋œ๋‹ค. The sensing means of this embodiment is composed of a plurality of sensing means (112, 114) having a mutually independent measurement method. Independent measurement means that each sensing means uses a different physical measurement principle, for example, the plurality of sensing means is composed of two sensors, a three-axis gyro sensor and a three-axis acceleration sensor.
์Ÿˆ์ด๋กœ์„ผ์„œ ๋˜๋Š” ๊ฐ€์†๋„์„ผ์„œ ๋ชจ๋‘ ์›€์ง์ž„์„ ๊ฐ์ง€ํ•˜๊ธฐ ์œ„ํ•ด ๊ด€์„ฑ๋ ฅ์„ ์ด์šฉํ•˜๋Š” ์„ผ์„œ์ด๋‹ค. ๊ทธ๋Ÿฌ๋‚˜, ์Ÿˆ์ด๋กœ์„ผ์„œ๋Š” ํšŒ์ „์šด๋™์„ ํ•˜๋Š” ์งˆ๋Ÿ‰์— ์ž‘์šฉํ•˜๋Š” ์ฝ”๋ฆฌ์˜ฌ๋ฆฌ์˜ ํž˜์„ ์ด์šฉํ•˜์—ฌ ๊ฐ์†๋„๋ฅผ ๊ฒ€์ถœํ•˜๋Š” ๋ฐฉ์‹์ธ๋ฐ ๋น„ํ•ด, ๊ฐ€์†๋„์„ผ์„œ๋Š” ์ง์„ ์šด๋™์„ ํ•˜๋Š” ์งˆ๋Ÿ‰์— ์ž‘์šฉํ•˜๋Š” ํž˜์„ ์ธก์ •ํ•˜๊ณ  ์šด๋™๋ฐฉ์ •์‹์„ ์ด์šฉํ•˜์—ฌ ๊ฐ€์†๋„๋ฅผ ๊ฒ€์ถœํ•˜๋Š” ๋ฐฉ์‹์ด๋‹ค. Both gyro and acceleration sensors use inertial forces to detect movement. However, the gyro sensor detects the angular velocity using the Coriolis force acting on the mass that rotates, whereas the acceleration sensor measures the force acting on the mass of linear movement and uses the equation of motion to measure the acceleration. It is a way of detection.
์ด๋Ÿฌํ•œ ๋‘๊ฐ€์ง€ ํž˜์€ ์™„์ „ํžˆ ๋‹ค๋ฅธ ๋ฌผ๋ฆฌ๋Ÿ‰์ด๊ธฐ ๋•Œ๋ฌธ์— ์Ÿˆ์ด๋กœ์„ผ์„œ ๋ฐ ๊ฐ€์†๋„์„ผ์„œ๋กœ ๊ฒ€์ถœํ•œ ์ขŒํ‘œ ๋ณ€์œ„๋Š” ๊ฐ๊ฐ ์™„์ „ํžˆ ๋…๋ฆฝ์ ์œผ๋กœ ๊ฒ€์ถœ๋˜๋Š” ๊ฒƒ์ด๋ฉฐ, ๊ฐ๊ฐ์˜ ์ขŒํ‘œ ๋ณ€์œ„๋ฅผ ์„œ๋กœ ๋น„๊ตํ•˜์—ฌ ๋ณด์ •ํ•˜๊ฒŒ ๋˜๋ฉด ํ•œ๊ฐ€์ง€ ์„ผ์„œ๋กœ๋งŒ ๊ฒ€์ถœํ•œ ์ขŒํ‘œ ๋ณ€์œ„์— ๋น„ํ•ด ์ƒ๋‹นํžˆ ๋†’์€ ์ •ํ™•๋„๋ฅผ ์–ป์„ ์ˆ˜ ์žˆ๊ฒŒ ๋œ๋‹ค. Since these two forces are completely different physical quantities, the coordinate displacements detected by the gyro sensor and the acceleration sensor are detected completely independently of each other. Comparing and correcting each of the coordinate displacements significantly compares with the coordinate displacements detected by only one sensor. High accuracy can be obtained.
๋ณธ ์‹ค์‹œ์˜ˆ์—์„œ๋Š” ๋ณ€์œ„๋Ÿ‰ ์—ฐ์‚ฐ์ˆ˜๋‹จ(220)์„ ํ†ตํ•ด ์ƒ๊ธฐ ๊ฐ ์„ผ์‹ฑ์ˆ˜๋‹จ์ด ์ธก์ •ํ•œ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„ ๋ฐ์ดํ„ฐ๋ฅผ ์ƒํ˜ธ ๋น„๊ตํ•˜์—ฌ ๋ณด์ •ํ•˜๋Š” ๊ธฐ๋Šฅ์ด ์ด๋ค„์ง„๋‹ค. In this embodiment, the displacement amount calculating means 220 performs a function of comparing and correcting the three-dimensional coordinate displacement data measured by the sensing means.
์ด๋Ÿฌํ•œ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„ ๋ฐ์ดํ„ฐ์˜ ์ƒํ˜ธ ๋น„๊ต ๋ฐ ๋ณด์ •์€, ๊ฐ ์„ผ์‹ฑ์ˆ˜๋‹จ์˜ ์ธก์ •๊ฐ’์˜ ํ—ˆ์šฉ๊ฐ€๋Šฅํ•œ ์˜ค์ฐจ๋ฒ”์œ„๋ฅผ ์„ค์ •ํ•œ ํ›„, ์ผ์ธก ์„ผ์‹ฑ์ˆ˜๋‹จ(112)์ด ์ธก์ •ํ•œ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„ ๋ฐ์ดํ„ฐ๋ฅผ ๊ธฐ์ค€์œผ๋กœ, ํƒ€์ธก ์„ผ์‹ฑ์ˆ˜๋‹จ(114)์ด ์ธก์ •ํ•œ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„ ๋ฐ์ดํ„ฐ ์ค‘ ์˜ค์ฐจ๋ฒ”์œ„๋ฅผ ๋„˜์–ด์„œ๋Š” ๊ธ‰๊ฒฉํžˆ ๋‹ค๋ฅธ ๊ฐ’์„ ๋‚˜ํƒ€๋‚ธ ๊ฒฝ์šฐ๋ฅผ ์—๋Ÿฌ๋กœ ํŒ๋‹จํ•˜์—ฌ ์ฒ˜๋ฆฌํ•˜๋Š” ๊ณผ์ •์„ ํ†ตํ•ด ์ด๋ค„์ง„๋‹ค. ์˜ค์ฐจ๋ฒ”์œ„ ์ด๋‚ด์˜ ๊ฐ ์„ผ์‹ฑ์ˆ˜๋‹จ์˜ ์ธก์ •๊ฐ’๋“ค์€ ํ‰๊ท ์„ ๋‚ด์–ด ๊ฒฐ๊ณผ๊ฐ’์œผ๋กœ ์ฑ„ํƒํ•œ๋‹ค. ๊ฐ ์„ผ์‹ฑ์ˆ˜๋‹จ์˜ ์ด๋Ÿฌํ•œ ์ „์ฒด ๊ณผ์ •์€ ๋„ 9์˜ S710 ๋‚ด์ง€ S730 ๋‹จ๊ณ„๋กœ ์ด๋ค„์ง„ ์ž‘๋™ํ๋ฆ„๋„๋ฅผ ํ†ตํ•ด ๋ณด๋‹ค ์ƒ์„ธํ•˜๊ฒŒ ์ดํ•ด๋  ์ˆ˜ ์žˆ๋‹ค. The mutual comparison and correction of the three-dimensional coordinate displacement data, after setting the allowable error range of the measured value of each sensing means, based on the three-dimensional coordinate displacement data measured by one sensing means 112, the other sensing means The case in which the three-dimensional coordinate displacement data measured by (114) shows a radically different value beyond the error range is determined through an error process. The measured values of each sensing means within the margin of error are averaged and taken as the result. This entire process of each sensing means can be understood in more detail through the operation flow chart consisting of the steps S710 to S730 of FIG.
์œ„์™€ ๊ฐ™์€ ์„ผ์‹ฑ์ˆ˜๋‹จ(112,114)์€ ์•ž์˜ ์‹ค์‹œ์˜ˆ์™€ ๋งˆ์ฐฌ๊ฐ€์ง€๋กœ 3์ถ•์˜ ์ขŒํ‘œ ๋ณ€์œ„๋ฅผ ์ธก์ •ํ•  ์ˆ˜๋งŒ ์žˆ์œผ๋ฉด, ์„ผ์‹ฑ์ˆ˜๋‹จ์˜ ๊ตฌ์กฐ๊ฐ€ ํŠน๋ณ„ํžˆ ์–ด๋Š ํ•œ๊ฐ€์ง€ ๊ตฌ์„ฑ์œผ๋กœ ์ œํ•œ์„ ๋ฐ›๋Š” ๊ฒƒ์€ ์•„๋‹ˆ๋‹ค. ๋˜ํ•œ, ๋ฐ˜๋“œ์‹œ 2๊ฐœ๋กœ ์ œํ•œ๋  ํ•„์š”๊ฐ€ ์—†์œผ๋ฉฐ ์„œ๋กœ ๋‹ค๋ฅธ ๋ฌผ๋ฆฌ์  ์ธก์ •์›๋ฆฌ๋ฅผ ์‚ฌ์šฉํ•˜๊ธฐ๋งŒ ํ•œ๋‹ค๋ฉด 2๊ฐœ ์ด์ƒ์œผ๋กœ ๊ตฌ๋น„๋  ์ˆ˜๋„ ์žˆ์Œ์€ ๋‹น์—ฐํ•˜๋‹ค. As described above, the sensing means 112 and 114 can measure the coordinate displacement of three axes as in the previous embodiment, and the structure of the sensing means is not particularly limited to any one configuration. In addition, it is not necessarily limited to two, it is natural that two or more may be provided as long as different physical measurement principles are used.
์•ž์˜ ์‹ค์‹œ์˜ˆ์™€ ์œ ์‚ฌํ•œ ๊ตฌ์„ฑ ๋ฐ ์ž‘๋™ํ๋ฆ„์— ๋Œ€ํ•ด์„œ๋Š” ์ค‘๋ณต ์„ค๋ช…์„ ์ƒ๋žตํ•œ๋‹ค. Duplicate description of the configuration and operation flow similar to the previous embodiment will be omitted.
๋„๋ฉด์„ ์ฐธ์กฐํ•˜์—ฌ ๋ณธ ๋ฐœ๋ช…์˜ ๋˜๋‹ค๋ฅธ ์‹ค์‹œ์˜ˆ์— ๋Œ€ํ•˜์—ฌ ์„ค๋ช…ํ•œ๋‹ค. ๋„ 10์€ ๋ณธ ๋ฐœ๋ช…์˜ ๋˜๋‹ค๋ฅธ ์‹ค์‹œ์˜ˆ์— ์˜ํ•œ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜์˜ ๊ตฌ์„ฑ๋„, ๋„ 11์€ ๋ณธ ๋ฐœ๋ช…์˜ ๋˜๋‹ค๋ฅธ ์‹ค์‹œ์˜ˆ์— ์˜ํ•œ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜์˜ ์ž‘๋™ํ๋ฆ„๋„์ด๋‹ค.Another embodiment of the present invention will be described with reference to the drawings. 10 is a block diagram of a ground displacement measuring apparatus according to another embodiment of the present invention, Figure 11 is a flow chart of the ground displacement measuring apparatus according to another embodiment of the present invention.
๋ณธ ์‹ค์‹œ์˜ˆ์—์„œ๋Š”, ์ด๋™๋ถ€(400)๊ฐ€ ๊ฒฝ์‚ฌ๊ด€ ๋‚ด์—์„œ ๊ทธ ๊ธธ์ด๋ฐฉํ–ฅ์œผ๋กœ ์ด๋™์‹œ ํƒ€์ด๋ฐ์„ค์ •์ˆ˜๋‹จ(210)์— ์˜ํ•ด ์„ค์ •๋œ ์ธก์ • ํƒ€์ด๋ฐ๋งˆ๋‹ค 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„๋ฅผ ์‹ค์‹œ๊ฐ„์œผ๋กœ ์ธก์ •ํ•˜๋Š” ์„ผ์‹ฑ์ˆ˜๋‹จ(110)๊ณผ ํ•จ๊ป˜, ๋ณด์กฐ ์„ผ์‹ฑ์ˆ˜๋‹จ(150)์ด ๋” ๊ตฌ๋น„๋œ๋‹ค. In this embodiment, the moving unit 400, along with the sensing means 110 for measuring in real time the three-dimensional coordinate displacement for each measurement timing set by the timing setting means 210 when moving in the longitudinal direction in the inclined tube, The sensing means 150 is further provided.
๋ณด์กฐ ์„ผ์‹ฑ์ˆ˜๋‹จ(150)์€ ์„ผ์‹ฑ์ˆ˜๋‹จ(110)์ด ์ธก์ •ํ•œ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„ ๋ฐ์ดํ„ฐ๋ฅผ ๋ณด์ •ํ•˜๋Š” ๊ธฐ๋Šฅ์„ ์ œ๊ณตํ•˜๋ฉฐ, ์ง€๋ฐ˜ ์ˆ˜์ง๋ฐฉํ–ฅ(z๋ฐฉํ–ฅ) ์ด๋™๊ฑฐ๋ฆฌ ์ธก์ •์„ผ์„œ(154) ๋˜๋Š” ์˜จ๋„์„ผ์„œ(156) ์ค‘์˜ ํ•˜๋‚˜ ๋˜๋Š” ๊ทธ ์กฐํ•ฉ์œผ๋กœ ๊ตฌ์„ฑ๋œ๋‹ค. The auxiliary sensing means 150 provides a function of correcting the three-dimensional coordinate displacement data measured by the sensing means 110, one of the ground vertical direction (z direction) moving distance measuring sensor 154 or the temperature sensor 156 Or combinations thereof.
์˜ˆ๋ฅผ ๋“ค์–ด, ๋„ 6์˜ ์‹ค์‹œ์˜ˆ์˜ ๊ฒฝ์šฐ, ์„ผ์‹ฑ์ˆ˜๋‹จ(110)์ด 3์ถ• ์Ÿˆ์ด๋กœ์„ผ์„œ ๋˜๋Š” 3์ถ• ๊ฐ€์†๋„์„ผ์„œ๋กœ ์ด๋ค„์ง€๋ฏ€๋กœ, ๋ณด์กฐ ์„ผ์‹ฑ์ˆ˜๋‹จ(150)์€ ์ง€๋ฐ˜ ์ˆ˜์ง๋ฐฉํ–ฅ(z๋ฐฉํ–ฅ) ์ด๋™๊ฑฐ๋ฆฌ ์ธก์ •์„ผ์„œ(154) ๋˜๋Š” ์˜จ๋„์„ผ์„œ(156) ์ค‘์˜ ํ•˜๋‚˜ ๋˜๋Š” ๊ทธ ์กฐํ•ฉ์œผ๋กœ ๊ตฌ์„ฑ๋œ๋‹ค. For example, in the case of the embodiment of Figure 6, since the sensing means 110 is made of a three-axis gyro sensor or three-axis acceleration sensor, the auxiliary sensing means 150 is a ground vertical direction (z direction) moving distance measuring sensor ( 154 or one or a combination of temperature sensors 156.
๋ฐ”๋žŒ์งํ•˜๊ฒŒ ๋ณด์กฐ ์„ผ์‹ฑ์ˆ˜๋‹จ(150)์€ ์ง€๋ฐ˜ ์ˆ˜์ง๋ฐฉํ–ฅ(z๋ฐฉํ–ฅ) ์ด๋™๊ฑฐ๋ฆฌ ์ธก์ •์„ผ์„œ(154) ๋ฐ ์˜จ๋„์„ผ์„œ(156) ๋ชจ๋‘๋ฅผ ๊ตฌ๋น„ํ•˜๋Š” ๊ฒƒ์ด ์ธก์ •์น˜์˜ ์ •๋ฐ€๋„๋ฅผ ๋†’์ด๋Š”๋ฐ ์ข‹๋‹ค.Preferably, the auxiliary sensing means 150 includes both the ground vertical direction (z direction) moving distance measuring sensor 154 and the temperature sensor 156 to increase the accuracy of the measured value.
๋„ 7์˜ ์‹ค์‹œ์˜ˆ์˜ ๊ฒฝ์šฐ, ์„ผ์‹ฑ์ˆ˜๋‹จ(110)์ด 2์ถ• ์Ÿˆ์ด๋กœ์„ผ์„œ ๋˜๋Š” 2์ถ• ๊ฐ€์†๋„์„ผ์„œ ์ค‘์˜ ์–ด๋Š ํ•˜๋‚˜์™€ ์ง€๋ฐ˜ ์ˆ˜์ง๋ฐฉํ–ฅ ์ด๋™๊ฑฐ๋ฆฌ ์ธก์ •์„ผ์„œ์˜ ์กฐํ•ฉ์œผ๋กœ ์ด๋ค„์ง€๋ฏ€๋กœ, ์˜จ๋„์„ผ์„œ(156) ๋งŒ์„ ๋ณด์กฐ ์„ผ์‹ฑ์ˆ˜๋‹จ(150)์œผ๋กœ ๊ตฌ๋น„ํ•˜๋ฉด ๋œ๋‹ค. In the case of the embodiment of Figure 7, since the sensing means 110 is made of a combination of any one of the two-axis gyro sensor or two-axis acceleration sensor and the ground vertical movement distance measuring sensor, only the temperature sensor 156 to the secondary sensing means ( 150).
์ด๋Ÿฌํ•œ ๊ตฌ์„ฑ์— ๋”ฐ๋ฅด๋ฉด, ์˜ˆ๋ฅผ ๋“ค์–ด ์Ÿˆ์ด๋กœ์„ผ์„œ ๋˜๋Š” ๊ฐ€์†๋„์„ผ์„œ๋กœ ๊ตฌ์„ฑ๋œ ์„ผ์‹ฑ์ˆ˜๋‹จ(110)๊ณผ ํ•จ๊ป˜, ๋‹ค์–‘ํ•œ ๋ฐฉ์‹์œผ๋กœ ์ธก์ •๊ฐ’์„ ๋ณด์ •ํ•ด์ฃผ๋Š” ๋ณด์กฐ ์„ผ์‹ฑ์ˆ˜๋‹จ(150)์„ ํ†ตํ•ด ๋ณด๋‹ค ์ •๋ฐ€๋„ ๋†’์€ ์ธก์ •์น˜๋ฅผ ์–ป์„ ์ˆ˜ ์žˆ๊ฒŒ ๋œ๋‹ค. According to this configuration, for example, together with the sensing means 110 composed of a gyro sensor or an acceleration sensor, more accurate measurement values can be obtained through the auxiliary sensing means 150 for correcting the measurement values in various ways.
์˜จ๋„์„ผ์„œ(156)๋Š” ์ธก์ • ๊ณผ์ • ์ค‘์— ์™ธ๋ถ€ ์˜จ๋„ ํ™˜๊ฒฝ์— ์˜ํ•ด ๋ฐœ์ƒ๋  ์ˆ˜ ์žˆ๋Š” ์Ÿˆ์ด๋กœ์„ผ์„œ ๋˜๋Š” ๊ฐ€์†๋„์„ผ์„œ์˜ ์ธก์ • ์˜ค์ฐจ๋ฅผ ๋ณด์ •ํ•ด์ฃผ๋Š” ๊ธฐ๋Šฅ์„ ํ•œ๋‹ค. The temperature sensor 156 serves to correct a measurement error of the gyro sensor or the acceleration sensor that may be generated by the external temperature environment during the measurement process.
๋ณธ ์‹ค์‹œ์˜ˆ์—์„œ ์‚ฌ์šฉ๋˜๋Š” ์Ÿˆ์ด๋กœ์„ผ์„œ ๋˜๋Š” ๊ฐ€์†๋„์„ผ์„œ๋Š” ์˜ˆ๋ฅผ ๋“ค์–ด, ์‹ค๋ฆฌ์ฝ˜ ์›จ์ดํผ๋‚˜ ๊ฐ์ข… ์ „๊ทน ๋˜๋Š” ์œ ์ „์ฒด๋ฐ•๋ง‰์„ ์ด์šฉํ•œ ๋‹ค์ธต๋ฐ•๋ง‰ ๊ตฌ์กฐ์ฒด๋กœ ํ˜•์„ฑ๋œ๋‹ค. The gyro sensor or the acceleration sensor used in this embodiment is formed of a multilayer thin film structure using, for example, a silicon wafer or various electrodes or dielectric thin films.
์ด๋Ÿฌํ•œ ๋‹ค์ธต๋ฐ•๋ง‰ ๊ตฌ์กฐ์ฒด์—์„œ ๊ฐ ๋ฐ•๋ง‰์€ ๋Œ€๋ถ€๋ถ„ ์™„์ „ํžˆ ๋‹ค๋ฅธ ์ž…์ž ๊ฒฐ์ •์ƒ์ˆ˜์™€ ๊ฒฐ์ •๊ฒฐํ•จ, ์—ดํŒฝ์ฐฝ ํŠน์„ฑ์„ ์ง€๋‹ˆ๊ธฐ ๋•Œ๋ฌธ์—, ์‹ค์˜จ์—์„œ๋Š” ๋ณ„ ์ฐจ์ด๊ฐ€ ์—†์ง€๋งŒ ๊ณ ์˜จ์—์„œ๋Š” ์ž”๋ฅ˜์‘๋ ฅ์ด ๋ฐœ์ƒํ•˜์—ฌ ๊ตฌ์กฐ์ฒด์— ๋ณ€์œ„๊ฐ€ ๋ฐœ์ƒํ•˜๊ฒŒ ๋œ๋‹ค. ๋ฐ•๋ง‰ ๊ตฌ์กฐ์ฒด์—์„œ์˜ ์ž”๋ฅ˜์‘๋ ฅ์˜ ๋ฐœ์ƒ ์›์ธ์œผ๋กœ์„œ๋Š” ๊ฒฐ์ •๊ฒฐํ•จ ๋˜๋Š” ๊ฒฐ์ •์ƒ์ˆ˜ ๋“ฑ ๊ธฐ๋ณธ์ ์ธ ๊ฒฐ์ •์ž…์ž์˜ ์ฐจ์ด์— ์˜ํ•ด ๋ฐœ์ƒํ•˜๋Š” ์ž”๋ฅ˜์‘๋ ฅ๊ณผ, ์˜จ๋„ ์ƒ์Šน ์‹œ ์—ดํŒฝ์ฐฝ ๊ณ„์ˆ˜๊ฐ€ ๊ฐ ์žฌ๋ฃŒ๋งˆ๋‹ค ๋‹ค๋ฅด๊ธฐ ๋•Œ๋ฌธ์— ๋ฐœ์ƒํ•˜๋Š” ์—ด์ž”๋ฅ˜ ์‘๋ ฅ ๋“ฑ์ด ์žˆ๋‹ค. ํŠนํžˆ, ์˜จ๋„ ์ƒ์Šน ์‹œ ๋ฐœ์ƒํ•˜๋Š” ์—ด์ž”๋ฅ˜ ์‘๋ ฅ์€ ์˜จ๋„์— ๋”ฐ๋ผ ๋งค์šฐ ํฐ ๊ฐ’(์ˆ˜๋ฐฑ GPa order)์„ ๋‚˜ํƒ€๋‚ผ ์ˆ˜ ์žˆ์œผ๋ฏ€๋กœ, ์Ÿˆ์ด๋กœ์„ผ์„œ ๋˜๋Š” ๊ฐ€์†๋„์„ผ์„œ์˜ ์˜จ๋„ ๋ณ€ํ™”์— ๋”ฐ๋ฅธ ์˜ค์ฐจ๊ฐ’์„ ๋ฐ์ดํ„ฐํ™”ํ•˜๊ณ  ์˜จ๋„์„ผ์„œ(156)๋ฅผ ํ†ตํ•ด ์ธก์ •๋œ ์˜จ๋„๊ฐ’์„ ์ด์šฉํ•˜์—ฌ ์˜ค์ฐจ๋ฅผ ๋ณด์ •ํ•˜๋Š” ๋ฐฉ์‹์„ ์ทจํ•˜๊ฒŒ ๋˜๋ฉด ์ธก์ •๊ฐ’์˜ ์ •๋ฐ€๋„๋ฅผ ๋”์šฑ ๋†’์ผ ์ˆ˜ ์žˆ๊ฒŒ ๋œ๋‹ค. In the multilayer thin film structure, since each thin film has almost completely different particle crystal constants, crystal defects, and thermal expansion characteristics, there is no difference at room temperature, but residual stress occurs at high temperatures, causing displacement of the structure. Residual stresses in the thin film structure include residual stresses caused by differences in basic crystal grains such as crystal defects or crystal constants, and thermal residual stresses generated because the coefficient of thermal expansion differs for each material during temperature rise. In particular, since the thermal residual stress generated when the temperature rises may represent a very large value (hundreds of GPa order) according to the temperature, the error value according to the temperature change of the gyro sensor or the acceleration sensor is dataged and the temperature sensor 156 is used. When the error is corrected using the measured temperature value, the accuracy of the measured value can be further increased.
์ด๋Ÿฌํ•œ ์ „์ฒด ๊ณผ์ •์€ ๋„ 11์˜ S910 ๋‚ด์ง€ S960 ๋‹จ๊ณ„๋กœ ์ด๋ค„์ง„ ์ž‘๋™ํ๋ฆ„๋„๋ฅผ ํ†ตํ•ด ๋ณด๋‹ค ์ƒ์„ธํ•˜๊ฒŒ ์ดํ•ด๋  ์ˆ˜ ์žˆ๋‹ค. . This entire process can be understood in more detail through the operation flow chart consisting of the steps S910 to S960 of FIG. .
์•ž์˜ ์‹ค์‹œ์˜ˆ์™€ ์œ ์‚ฌํ•œ ๊ตฌ์„ฑ ๋ฐ ์ž‘๋™ํ๋ฆ„์— ๋Œ€ํ•ด์„œ๋Š” ์ค‘๋ณต ์„ค๋ช…์„ ์ƒ๋žตํ•œ๋‹ค. Duplicate description of the configuration and operation flow similar to the previous embodiment will be omitted.
๋„๋ฉด์„ ์ฐธ์กฐํ•˜์—ฌ ๋ณธ ๋ฐœ๋ช…์˜ ๋˜๋‹ค๋ฅธ ์‹ค์‹œ์˜ˆ์— ๋Œ€ํ•˜์—ฌ ์„ค๋ช…ํ•œ๋‹ค. Another embodiment of the present invention will be described with reference to the drawings.
๋„ 12๋Š” ๋ณธ ๋ฐœ๋ช…์˜ ๋˜๋‹ค๋ฅธ ์‹ค์‹œ์˜ˆ์— ์˜ํ•œ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜์˜ ๊ตฌ์„ฑ๋„, ๋„ 13์€ ๋ณธ ๋ฐœ๋ช…์˜ ๋˜๋‹ค๋ฅธ ์‹ค์‹œ์˜ˆ์— ์˜ํ•œ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜์˜ ์ž‘๋™ํ๋ฆ„๋„์ด๋‹ค. 12 is a block diagram of a ground displacement measuring apparatus according to another embodiment of the present invention, Figure 13 is a flow chart of the ground displacement measuring apparatus according to another embodiment of the present invention.
๋ณธ ์‹ค์‹œ์˜ˆ์—์„œ ํƒ€์ด๋ฐ์„ค์ •์ˆ˜๋‹จ(210)์€ ์ƒํ˜ธ ๋…๋ฆฝ์ ์ธ ๋ณต์ˆ˜์˜ ์ฃผํŒŒ์ˆ˜๋ฅผ ์ธก์ • ํƒ€์ด๋ฐ์œผ๋กœ ์„ค์ •ํ•  ์ˆ˜ ์žˆ๋„๋ก ๊ตฌ๋น„๋˜์–ด, ๋ณต์ˆ˜์˜ ์ด๋™ ์ธก์ • ๊ณผ์ •๋ณ„๋กœ ์„œ๋กœ ๋‹ค๋ฅธ ์ฃผํŒŒ์ˆ˜๊ฐ’์„ ์ธก์ • ํƒ€์ด๋ฐ์œผ๋กœ ์„ค์ •ํ•˜๊ณ , ๊ฐ ์ด๋™ ์ธก์ • ๊ณผ์ •๋ณ„๋กœ ์„ผ์‹ฑ์ˆ˜๋‹จ(112,114)์ด ์ธก์ •ํ•œ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„ ๋ฐ์ดํ„ฐ๋ฅผ ์ƒํ˜ธ ๋น„๊ตํ•˜์—ฌ ๋ณด์ •ํ•˜๋Š” ๊ธฐ๋Šฅ์„ ๊ตฌ๋น„ํ•œ๋‹ค. In the present embodiment, the timing setting means 210 is provided to set a plurality of independent frequencies as the measurement timing, set different frequency values as the measurement timings for each of the plurality of movement measuring processes, and sense each sensing measurement process. And means for comparing and correcting the three-dimensional coordinate displacement data measured by the means 112,114.
์˜ˆ๋ฅผ ๋“ค์–ด, ์ด๋™๋ถ€(400)๋ฅผ ๋ณต์ˆ˜ํšŒ ์ด๋™์‹œํ‚ค๋ฉด์„œ ์ธก์ •ํ•˜๋˜, ์ฒซ๋ฒˆ์งธ ์ด๋™ ์ธก์ •์‹œ์—๋Š” ์„ผ์‹ฑ์ˆ˜๋‹จ(112,114)์˜ ์ธก์ • ํƒ€์ด๋ฐ์„ 25Hz๋กœ ์„ค์ •ํ•˜์—ฌ ์ธก์ •์„ ์‹ค์‹œํ•˜๊ณ , ๋‘ ๋ฒˆ์งธ ์ด๋™ ์ธก์ •์‹œ์—๋Š” ์„ผ์‹ฑ์ˆ˜๋‹จ(112,114)์˜ ์ธก์ • ํƒ€์ด๋ฐ์„ 100Hz๋กœ ์„ค์ •ํ•˜์—ฌ ์ธก์ •์„ ์‹ค์‹œํ•˜์—ฌ, ์ฒซ๋ฒˆ์งธ ์ธก์ •์‹œ์™€ ๋‘๋ฒˆ์งธ ์ธก์ •์‹œ์˜ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„๋ฅผ ์ƒํ˜ธ ๋น„๊ตํ•˜์—ฌ ๋ณด์ •ํ•˜๋Š” ๊ฒƒ์ด๋‹ค. For example, the measurement is performed while moving the moving unit 400 a plurality of times, and the measurement is performed by setting the measurement timing of the sensing means 112 and 114 to 25 Hz during the first movement measurement, and the sensing means 112 and 114 during the second movement measurement. The measurement timing is set to 100 Hz, and the three-dimensional coordinate displacements of the first measurement and the second measurement are compared and corrected.
๋™์ผํ•œ ์ด๋™ ์†๋„๋ฅผ ์œ ์ง€ํ•œ ์ƒํƒœ์—์„œ ์ดˆ๋‹น 25๋ฒˆ ์ธก์ •ํ•˜๋Š” ๊ฒฝ์šฐ์™€ ์ดˆ๋‹น 100๋ฒˆ ์ธก์ •ํ•˜๋Š” ๊ฒฝ์šฐ๋ฅผ ๋น„๊ตํ•˜๋ฉด, ํฐ ๊ณก๋ฅ ๋ฐ˜๊ฒฝ์—์„œ๋Š” ์ดˆ๋‹น 25๋ฒˆ ์ธก์ •ํ•˜๋Š” ๊ฒƒ์œผ๋กœ๋„ ๋น„๊ต์  ์ •ํ™•ํ•œ ๊ฐ’์„ ์–ป์„ ์ˆ˜ ์žˆ์œผ๋ฉฐ, ์ž‘์€ ๊ณก๋ฅ ๋ฐ˜๊ฒฝ์—์„œ๋Š” ์ดˆ๋‹น 100๋ฒˆ ์ธก์ •ํ•˜๋Š” ์ •๋„์˜ ๋†’์€ ์ฃผํŒŒ์ˆ˜๋ฅผ ์‚ฌ์šฉํ•  ๋•Œ ๋”์šฑ ์ •ํ™•ํ•œ ๊ฐ’์„ ์–ป์„ ์ˆ˜ ์žˆ๋‹ค. Comparing 25 measurements per second with 100 measurements per second while maintaining the same movement speed, 25 measurements per second can be obtained with a large radius of curvature and 100 seconds per second with a small radius of curvature. More accurate values can be obtained when using a frequency that is high enough to measure twice.
๊ณก๋ฅ ๋ฐ˜๊ฒฝ์— ๋”ฐ๋ผ ์—ฐ์‚ฐ ์‹œ ๋ฐ์ดํ„ฐ์˜ ์‹ ๋ขฐ๋„(์‹ ๋ขฐ๋„ ๊ณ„์ˆ˜ ๋˜๋Š” ๊ฐ€์ค‘์น˜)๋ฅผ ์กฐ์ ˆํ•˜์—ฌ ์ „์ฒด ๋ฐ์ดํ„ฐ์˜ ์‹ ๋ขฐ์„ฑ์„ ํ–ฅ์ƒ์‹œํ‚ฌ ์ˆ˜๋„ ์žˆ๋‹ค. ์˜ˆ๋ฅผ ๋“ค๋ฉด, ์ž‘์€ ๊ณก๋ฅ ๋ฐ˜๊ฒฝ์—์„œ๋Š” ๋†’์€ ์ฃผํŒŒ์ˆ˜์˜ ๋ฐ์ดํ„ฐ์— ๋†’์€ ์‹ ๋ขฐ๋„๋ฅผ ๋ถ€์—ฌํ•˜๊ณ , ๊ทธ ๋ฐ˜๋Œ€์˜ ๊ฒฝ์šฐ์—๋Š” ๋‚ฎ์€ ์ฃผํŒŒ์ˆ˜์˜ ๋ฐ์ดํ„ฐ์— ๋†’์€ ์‹ ๋ขฐ๋„๋ฅผ ๋ถ€์—ฌํ•˜์—ฌ, ๋ณ€์œ„์—ฐ์‚ฐ์— ์ด๋Ÿฌํ•œ ์‹ ๋ขฐ๋„๋ฅผ ๋ฐ˜์˜ํ•˜๊ฒŒ ๋˜๋ฉด, ์ข€ ๋” ์ •ํ™•ํ•œ ์—ฐ์‚ฐ์ด ๊ฐ€๋Šฅํ•˜๊ฒŒ ๋œ๋‹ค. Depending on the radius of curvature, the reliability of the data (reliability coefficient or weight) may be adjusted to improve the reliability of the entire data. For example, if a small curvature radius gives high reliability to high frequency data, and vice versa, high reliability to low frequency data and reflects this reliability in the displacement operation, a more accurate calculation It becomes possible.
์ด๋Ÿฌํ•œ ์—ฐ์‚ฐ๊ณผ์ •์„ ์ข€ ๋” ๊ตฌ์ฒด์ ์œผ๋กœ ์˜ˆ์‹œํ•˜๋ฉด ๋‹ค์Œ๊ณผ ๊ฐ™๋‹ค. More specifically, the calculation process is as follows.
๊ณก๋ฅ ๋ฐ˜๊ฒฝ์˜ ๊ณ ์ €(้ซ˜ไฝŽ)๋ฅผ ๊ฒฐ์ •ํ•˜๋Š” ๊ธฐ์ค€๊ฐ’์„ ์„ค์ •ํ•œ ํ›„, ๋†’์€ ์ฃผํŒŒ์ˆ˜์—์„œ ์–ป์€ ๋ฐ์ดํ„ฐ์™€ ๋‚ฎ์€ ์ฃผํŒŒ์ˆ˜์—์„œ ์–ป์€ ๋ฐ์ดํ„ฐ(ํŠน์ • ์ง€์ ์˜ ์ขŒํ‘œ ๋ณ€์œ„๊ฐ’)๋ฅผ ๊ฐ๊ฐ A, B๋ผ๊ณ  ํ•˜๋ฉด, ๊ณก๋ฅ ๋ฐ˜๊ฒฝ์„ ๋ฐ˜์˜ํ•œ ์ธก์ • ๋ฐ์ดํ„ฐ์˜ ํ‰๊ท ๊ฐ’(a)์€ ๋‹ค์Œ๊ณผ ๊ฐ™์ด ๊ตฌํ•ด์งˆ ์ˆ˜ ์žˆ๋‹ค. After setting the reference value for determining the high and low radius of curvature, A and B data obtained at high frequency and low frequency (coordinate displacement of a specific point) are A and B, respectively. The average value a can be obtained as follows.
[์‹ 1][Equation 1]
Figure PCTKR2009006204-appb-I000001
Figure PCTKR2009006204-appb-I000001
[์‹ 2][Equation 2]
Figure PCTKR2009006204-appb-I000002
Figure PCTKR2009006204-appb-I000002
์ƒ๊ธฐ [์‹ 1]์—์„œ, n์€ ๋ฐ์ดํ„ฐ์˜ ์ด ๊ฐฏ์ˆ˜์ด๊ณ , ฯA, ฯB๋Š” ๊ฐ๊ฐ A, B ๊ฐ’์˜ ์‹ ๋ขฐ๋„ ๊ณ„์ˆ˜๋ฅผ ๋‚˜ํƒ€๋‚ด๋ฉฐ, ์ด๋Š” ๊ณก๋ฅ ๋ฐ˜๊ฒฝ์„ ๋ฐ˜์˜ํ•˜์—ฌ ๊ฒฐ์ •๋œ๋‹ค. In Equation 1, n is the total number of data, ฯ A , ฯ B represents the reliability coefficient of the A, B value, respectively, which is determined to reflect the radius of curvature.
์˜ˆ๋ฅผ ๋“ค๋ฉด, A๊ฐ’์ด 110์ด๊ณ  B๊ฐ’์ด 90์ผ ๊ฒฝ์šฐ ํ‰๊ท ๊ฐ’์€ 100์ด ๋˜๋Š”๋ฐ, ๋น„๊ต์  ์ž‘์€ ๊ณก๋ฅ ๋ฐ˜๊ฒฝ์˜ ์กฐ๊ฑด์ด๋ผ๋ฉด, A๊ฐ’์— ์ข€ ๋” ๋†’์€ ์‹ ๋ขฐ๋„๋ฅผ ๋ฐ˜์˜ํ•˜๊ธฐ ์œ„ํ•ด ฯA์„ 1.8, ฯB์„ 0.2๋กœ ์„ค์ •ํ•œ๋‹ค๋ฉด ๊ฒฐ๊ณผ๊ฐ’์€ 108์ด ๋œ๋‹ค. ๋‹จ, ์‹ ๋ขฐ๋„๊ณ„์ˆ˜์˜ ์„ค์ •์— ์žˆ์–ด์„œ๋Š”, ์œ„์˜ [์‹ 2]์˜ ์กฐ๊ฑด์„ ๋งŒ์กฑํ•˜๋„๋ก ํ•œ๋‹ค. For example, if the value of A is 110 and the value of B is 90, the average value is 100. If the condition is a relatively small radius of curvature, ฯ A is set to 1.8 and ฯ B is set to 0.2 to reflect higher reliability in the A value. If set, the result is 108. However, in setting the reliability coefficient, the condition of the above [Equation 2] is satisfied.
์œ„ ์˜ˆ์—์„œ A, B ๊ฐ’์€ ๊ฐ๊ฐ ๋‹ค๋ฅธ ์ฃผํŒŒ์ˆ˜๋กœ ์„ค์ •๋œ ์ƒํƒœ์—์„œ ๊ฐ๊ฐ ์ธก์ •๋œ ํŠน์ • ์ง€์ ์˜ ์ขŒํ‘œ ๋ณ€์œ„๊ฐ’์œผ๋กœ์„œ, ์ฃผํŒŒ์ˆ˜ ์„ค์ • ์ƒํƒœ์— ๋”ฐ๋ผ ์ธก์ • ์ง€์ ์ด ์‹ค์ œ๋กœ ์ผ์น˜ํ•˜๋Š” 2๊ฐœ์˜ ์ธก์ •๊ฐ’์„ ์ง์ ‘ ๋น„๊ตํ•  ์ˆ˜๋„ ์žˆ์ง€๋งŒ, ์ „์ฒด ์ธก์ • ๊ฒฝ๋กœ์— ๊ฑธ์ณ ๊ฐ ์ฃผํŒŒ์ˆ˜๋ณ„๋กœ ์ด์‚ฐ ๋ฐ์ดํ„ฐ ํ˜•ํƒœ๋กœ ์–ป์–ด์ง„ ์ง€๋ฐ˜ ๋ณ€์œ„๊ฐ’์„ ๋ณด๊ฐ„ ์—ฐ์‚ฐ์„ ํ†ตํ•ด ์—ฐ์† ๋ฐ์ดํ„ฐ ํ˜•ํƒœ๋กœ ๊ตฌํ•œ ํ›„, ์ž‘์—…์ž์— ์˜ํ•ด ์„ค์ •๋œ ์†Œ์ •์˜ ์ง€์ ๋ณ„๋กœ ๋น„๊ตํ•˜๋Š” ๋ฐฉ์‹์„ ์ทจํ•  ์ˆ˜๋„ ์žˆ๋‹ค. In the above example, the A and B values are the coordinate displacement values of the specific points measured at different frequencies, but the two measurement values where the measurement points are actually matched according to the frequency setting state can be directly compared. Ground displacement values obtained in discrete data form for each frequency over a range may be obtained in the form of continuous data through interpolation, and then compared for each predetermined point set by an operator.
๊ฒฝ์‚ฌ๊ด€(500)์˜ ๊ฒฝ์‚ฌ๋ณ€ํ™”๋Š” ์ธก์ • ์ „์—๋Š” ์ •ํ™•ํžˆ ์•Œ ์ˆ˜ ์—†์œผ๋ฏ€๋กœ, ์ฃผํŒŒ์ˆ˜๋ฅผ ๋‹ฌ๋ฆฌํ•˜์—ฌ ๋ณต์ˆ˜ํšŒ ์ธก์ •์„ ์‹ค์‹œํ•˜๊ณ , ์œ„์™€ ๊ฐ™์€ ๋ฐฉ์‹์œผ๋กœ ์ธก์ •๊ฐ’์„ ๋ณด์ •ํ•จ์— ๋”ฐ๋ผ ์˜ค์ฐจ๋ฅผ ์ค„์ด๊ณ  ์ •ํ™•๋„๋ฅผ ๋†’์ผ ์ˆ˜ ์žˆ๋‹ค. Since the inclination change of the inclined tube 500 may not be accurately known before the measurement, the measurement may be performed a plurality of times by varying the frequency, and the error may be reduced and the accuracy may be increased by correcting the measured value in the above manner.
์ธก์ • ํƒ€์ด๋ฐ์œผ๋กœ ์„ค์ •ํ•  ์ˆ˜ ์žˆ๋Š” ์ฃผํŒŒ์ˆ˜๋Š” 1-100Hz ์˜ ๋ฒ”์œ„๊ฐ€ ๋ฐ”๋žŒ์งํ•˜๋ฉฐ, ํƒ€์ด๋ฐ ์„ค์ •์ˆ˜๋‹จ(210)์— ์˜ํ•ด ์ „์ž์ ์œผ๋กœ ์ œ์–ด ๊ฐ€๋Šฅํ•˜๋‹ค. The frequency that can be set as the measurement timing is preferably in the range of 1-100 Hz, and can be electronically controlled by the timing setting means 210.
3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„ ๋ฐ์ดํ„ฐ์˜ ์ƒํ˜ธ ๋น„๊ต ๋ฐ ๋ณด์ •์€, ํ•˜๋‚˜์˜ ์ฃผํŒŒ์ˆ˜๋ฅผ ์ธก์ • ํƒ€์ด๋ฐ์œผ๋กœ ์„ค์ •ํ•˜์—ฌ ์ธก์ •ํ•œ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„ ๋ฐ์ดํ„ฐ๋ฅผ ๊ธฐ์ค€์œผ๋กœ, ๋˜๋‹ค๋ฅธ ์ฃผํŒŒ์ˆ˜๋ฅผ ์ธก์ • ํƒ€์ด๋ฐ์œผ๋กœ ์„ค์ •ํ•˜์—ฌ ์ธก์ •ํ•œ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„ ๋ฐ์ดํ„ฐ ์ค‘ ๊ธฐ์„ค์ •๋œ ์˜ค์ฐจ๋ฒ”์œ„๋ฅผ ๋„˜์–ด์„œ๋Š” ๊ฐ’์„ ๋‚˜ํƒ€๋‚ธ ๊ฒฝ์šฐ๋ฅผ ์—๋Ÿฌ๋กœ ํŒ๋‹จํ•˜์—ฌ ์ฒ˜๋ฆฌํ•˜๋Š” ๊ณผ์ •์„ ํ†ตํ•ด ์ด๋ค„์ง„๋‹ค. ์ด๋Ÿฌํ•œ ์ „์ฒด ๊ณผ์ •์€ ๋„ 13์˜ S1010 ๋‚ด์ง€ S1080 ๋‹จ๊ณ„๋กœ ์ด๋ค„์ง„ ์ž‘๋™ํ๋ฆ„๋„๋ฅผ ํ†ตํ•ด ๋ณด๋‹ค ์ƒ์„ธํ•˜๊ฒŒ ์ดํ•ด๋  ์ˆ˜ ์žˆ๋‹ค. The mutual comparison and correction of the three-dimensional coordinate displacement data is based on the three-dimensional coordinate displacement data measured by setting one frequency as the measurement timing, and among the three-dimensional coordinate displacement data measured by setting another frequency as the measurement timing. This is done through the process of judging the case where the value is over the set error range as an error. This entire process can be understood in more detail through the operation flow chart consisting of the steps S1010 to S1080 of FIG.
ํ•œํŽธ, ๋ณธ ์‹ค์‹œ์˜ˆ์— ์žˆ์–ด์„œ๋„, ์ง€๋ฐ˜ ์ˆ˜์ง๋ฐฉํ–ฅ ์ด๋™๊ฑฐ๋ฆฌ ์ธก์ •์„ผ์„œ(154) ๋˜๋Š” ์˜จ๋„์„ผ์„œ(156) ์ค‘์˜ ์ ์–ด๋„ ์–ด๋Š ํ•˜๋‚˜๋ฅผ ๋ณด์กฐ ์„ผ์‹ฑ์ˆ˜๋‹จ(150)์œผ๋กœ ๋” ๊ตฌ๋น„ํ•˜์—ฌ, ์„ผ์‹ฑ์ˆ˜๋‹จ(112,114)์ด ์ธก์ •ํ•œ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„ ๋ฐ์ดํ„ฐ๋ฅผ ๋ณด์ •ํ•˜๋Š” ๊ธฐ๋Šฅ์„ ๊ตฌ๋น„ํ•˜๋„๋ก ํ•˜์—ฌ, ์ธก์ • ์ •๋ฐ€๋„๋ฅผ ๋”์šฑ ๋†’์ด๋Š” ํšจ๊ณผ๋ฅผ ์–ป์„ ์ˆ˜ ์žˆ๋‹ค. On the other hand, also in this embodiment, at least one of the ground vertical movement distance measuring sensor 154 or the temperature sensor 156 is further provided as the auxiliary sensing means 150, the three-dimensional measured by the sensing means (112, 114) By providing the function of correcting the coordinate displacement data, the effect of further increasing the measurement accuracy can be obtained.
์•ž์˜ ์‹ค์‹œ์˜ˆ์™€ ์œ ์‚ฌํ•œ ๊ตฌ์„ฑ ๋ฐ ์ž‘๋™ํ๋ฆ„์— ๋Œ€ํ•ด์„œ๋Š” ์ค‘๋ณต ์„ค๋ช…์„ ์ƒ๋žตํ•œ๋‹ค. Duplicate description of the configuration and operation flow similar to the previous embodiment will be omitted.
๋„๋ฉด์„ ์ฐธ์กฐํ•˜์—ฌ ๋ณธ ๋ฐœ๋ช…์˜ ๋˜๋‹ค๋ฅธ ์‹ค์‹œ์˜ˆ์— ๋Œ€ํ•˜์—ฌ ์„ค๋ช…ํ•œ๋‹ค. Another embodiment of the present invention will be described with reference to the drawings.
๋„ 14๋Š” ๋ณธ ๋ฐœ๋ช…์˜ ๋˜๋‹ค๋ฅธ ์‹ค์‹œ์˜ˆ์— ์˜ํ•œ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜์˜ ์ž‘๋™ํ๋ฆ„๋„์ด๋‹ค. 14 is an operation flowchart of the ground displacement measuring apparatus according to another embodiment of the present invention.
๋ณธ ์‹ค์‹œ์˜ˆ์—์„œ ์„ผ์‹ฑ์ˆ˜๋‹จ์€ ๋ณต์ˆ˜์˜ ์„ผ์‹ฑ์ˆ˜๋‹จ(112,114)์œผ๋กœ ๊ตฌ์„ฑ๋˜๋ฉฐ, ํƒ€์ด๋ฐ์„ค์ •์ˆ˜๋‹จ(210)์€ ๊ฐ ์„ผ์‹ฑ์ˆ˜๋‹จ๋ณ„๋กœ ์ƒํ˜ธ ๋…๋ฆฝ์ ์ธ ๋ณต์ˆ˜์˜ ์ฃผํŒŒ์ˆ˜๋ฅผ ์ธก์ • ํƒ€์ด๋ฐ์œผ๋กœ ์„ค์ •ํ•  ์ˆ˜ ์žˆ๋„๋ก ๊ตฌ๋น„๋˜์–ด, ๊ฐ ์„ผ์‹ฑ์ˆ˜๋‹จ(112,114)์ด ์ธก์ •ํ•œ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„ ๋ฐ์ดํ„ฐ๋ฅผ ์ƒํ˜ธ ๋น„๊ตํ•˜์—ฌ ๋ณด์ •ํ•˜๋Š” ๊ธฐ๋Šฅ์„ ๊ตฌ๋น„ํ•œ๋‹ค.In the present embodiment, the sensing means is composed of a plurality of sensing means (112, 114), the timing setting means 210 is provided to set a plurality of frequencies independent of each sensing means for each of the sensing means, each sensing means (112,114) ) Compares and corrects the three-dimensional coordinate displacement data measured by
์˜ˆ๋ฅผ ๋“ค์–ด, ์ด๋™๋ถ€(400)๋ฅผ ์ด๋™์‹œํ‚ค๋ฉด์„œ ์ธก์ •ํ•˜๋˜, ์ œ1์„ผ์‹ฑ์ˆ˜๋‹จ(112)์˜ ์ธก์ • ํƒ€์ด๋ฐ์€ 25Hz๋กœ ์„ค์ •ํ•˜๊ณ , ์ œ2์„ผ์‹ฑ์ˆ˜๋‹จ(114)์˜ ์ธก์ • ํƒ€์ด๋ฐ์€ 100Hz๋กœ ์„ค์ •ํ•˜์—ฌ ์ธก์ •์„ ์‹ค์‹œํ•˜๊ณ , ์ œ1์„ผ์‹ฑ์ˆ˜๋‹จ(112)์ด ์ธก์ •ํ•œ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„์™€ ์ œ2์„ผ์‹ฑ์ˆ˜๋‹จ(114)์ด ์ธก์ •ํ•œ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„๋ฅผ ์ƒํ˜ธ ๋น„๊ตํ•˜์—ฌ ๋ณด์ •ํ•˜๋Š” ๊ฒƒ์ด๋‹ค.For example, while measuring while moving the moving unit 400, the measurement timing of the first sensing means 112 is set to 25 Hz, the measurement timing of the second sensing means 114 is set to 100 Hz to perform the measurement In this case, the three-dimensional coordinate displacement measured by the first sensing means 112 and the three-dimensional coordinate displacement measured by the second sensing means 114 are compared and corrected.
์ด๋Ÿฌํ•œ ๋ฐฉ์‹์— ๋”ฐ๋ฅด๋ฉด, 1ํšŒ์˜ ์ธก์ •์—๋„ ์•ž์˜ ์‹ค์‹œ์˜ˆ์™€ ๊ฐ™์€ ๋ณต์ˆ˜์˜ ์ฃผํŒŒ์ˆ˜ ์ธก์ • ํšจ๊ณผ๋ฅผ ์–ป์„ ์ˆ˜ ์žˆ๊ฒŒ ๋œ๋‹ค. ์ œ1์„ผ์‹ฑ์ˆ˜๋‹จ(112)๊ณผ ์ œ2์„ผ์‹ฑ์ˆ˜๋‹จ(114)์€ ๋ฐ˜๋“œ์‹œ ๋™์ผํ•œ ์ข…๋ฅ˜์˜ ์„ผ์„œ๋ฅผ ์‚ฌ์šฉํ•  ํ•„์š”๋Š” ์—†์œผ๋ฉฐ, ๋‹ค๋ฅธ ์ข…๋ฅ˜์˜ ์„ผ์„œ๋ฅผ ์‚ฌ์šฉํ•  ์ˆ˜๋„ ์žˆ๋‹ค. According to this method, a plurality of frequency measuring effects as in the previous embodiment can be obtained even in one measurement. The first sensing means 112 and the second sensing means 114 do not necessarily use the same type of sensor, but may use other types of sensors.
์ด๋Ÿฌํ•œ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„ ๋ฐ์ดํ„ฐ์˜ ์ƒํ˜ธ ๋น„๊ต ๋ฐ ๋ณด์ •์€, ํ•˜๋‚˜์˜ ์ฃผํŒŒ์ˆ˜๋ฅผ ์ธก์ • ํƒ€์ด๋ฐ์œผ๋กœ ์„ค์ •ํ•˜์—ฌ ์ธก์ •ํ•œ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„ ๋ฐ์ดํ„ฐ๋ฅผ ๊ธฐ์ค€์œผ๋กœ, ๋˜๋‹ค๋ฅธ ์ฃผํŒŒ์ˆ˜๋ฅผ ์ธก์ • ํƒ€์ด๋ฐ์œผ๋กœ ์„ค์ •ํ•˜์—ฌ ์ธก์ •ํ•œ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„ ๋ฐ์ดํ„ฐ ์ค‘ ๊ธฐ์„ค์ •๋œ ์˜ค์ฐจ๋ฒ”์œ„๋ฅผ ๋„˜์–ด์„œ๋Š” ๊ฐ’์„ ๋‚˜ํƒ€๋‚ธ ๊ฒฝ์šฐ๋ฅผ ์—๋Ÿฌ๋กœ ํŒ๋‹จํ•˜์—ฌ ์ฒ˜๋ฆฌํ•˜๋Š” ๊ณผ์ •์„ ํ†ตํ•ด ์ด๋ค„์ง„๋‹ค. ์ด๋Ÿฌํ•œ ์ „์ฒด ๊ณผ์ •์€ ๋„ 14์˜ S1210 ๋‚ด์ง€ S1280 ๋‹จ๊ณ„๋กœ ์ด๋ค„์ง„ ์ž‘๋™ํ๋ฆ„๋„๋ฅผ ํ†ตํ•ด ๋ณด๋‹ค ์ƒ์„ธํ•˜๊ฒŒ ์ดํ•ด๋  ์ˆ˜ ์žˆ๋‹ค. The mutual comparison and correction of the three-dimensional coordinate displacement data is based on the three-dimensional coordinate displacement data measured by setting one frequency as the measurement timing, and among the three-dimensional coordinate displacement data measured by setting another frequency as the measurement timing. The case in which a value exceeding a preset error range is determined as an error is made through a process of processing. This entire process can be understood in more detail through the operation flow chart consisting of the steps S1210 to S1280 of FIG.
ํ•œํŽธ, ๋ณธ ์‹ค์‹œ์˜ˆ์— ์žˆ์–ด์„œ๋„, ์ง€๋ฐ˜ ์ˆ˜์ง๋ฐฉํ–ฅ ์ด๋™๊ฑฐ๋ฆฌ ์ธก์ •์„ผ์„œ(154) ๋˜๋Š” ์˜จ๋„์„ผ์„œ(156) ์ค‘์˜ ์ ์–ด๋„ ์–ด๋Š ํ•˜๋‚˜๋ฅผ ๋ณด์กฐ ์„ผ์‹ฑ์ˆ˜๋‹จ(150)์œผ๋กœ ๋” ๊ตฌ๋น„ํ•˜์—ฌ, ์„ผ์‹ฑ์ˆ˜๋‹จ(112,114)์ด ์ธก์ •ํ•œ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„ ๋ฐ์ดํ„ฐ๋ฅผ ๋ณด์ •ํ•˜๋Š” ๊ธฐ๋Šฅ์„ ๊ตฌ๋น„ํ•˜๋„๋ก ํ•˜์—ฌ, ์ธก์ • ์ •๋ฐ€๋„๋ฅผ ๋”์šฑ ๋†’์ด๋Š” ํšจ๊ณผ๋ฅผ ์–ป์„ ์ˆ˜ ์žˆ๋‹ค. On the other hand, also in this embodiment, at least one of the ground vertical movement distance measuring sensor 154 or the temperature sensor 156 is further provided as the auxiliary sensing means 150, the three-dimensional measured by the sensing means (112, 114) By providing the function of correcting the coordinate displacement data, the effect of further increasing the measurement accuracy can be obtained.
์•ž์˜ ์‹ค์‹œ์˜ˆ์™€ ์œ ์‚ฌํ•œ ๊ตฌ์„ฑ ๋ฐ ์ž‘๋™ํ๋ฆ„์— ๋Œ€ํ•ด์„œ๋Š” ์ค‘๋ณต ์„ค๋ช…์„ ์ƒ๋žตํ•œ๋‹ค. Duplicate description of the configuration and operation flow similar to the previous embodiment will be omitted.
์ด์ƒ ์„ค๋ช…ํ•œ ๋ณธ ๋ฐœ๋ช…์€ ๊ทธ ๊ธฐ์ˆ ์  ์‚ฌ์ƒ ๋˜๋Š” ์ฃผ์š”ํ•œ ํŠน์ง•์œผ๋กœ๋ถ€ํ„ฐ ๋ฒ—์–ด๋‚จ์ด ์—†์ด ๋‹ค๋ฅธ ์—ฌ๋Ÿฌ๊ฐ€์ง€ ํ˜•ํƒœ๋กœ ์‹ค์‹œ๋  ์ˆ˜ ์žˆ๋‹ค. ๋”ฐ๋ผ์„œ, ์ƒ๊ธฐ ์‹ค์‹œ์˜ˆ๋Š” ๋ชจ๋“  ์ ์—์„œ ๋‹จ์ˆœํ•œ ์˜ˆ์‹œ์— ์ง€๋‚˜์ง€ ์•Š์œผ๋ฉฐ ํ•œ์ •์ ์œผ๋กœ ํ•ด์„๋˜์–ด์„œ๋Š” ์•ˆ๋œ๋‹ค.The present invention described above can be embodied in many different forms without departing from the spirit or main features thereof. Therefore, the above embodiments are merely examples in all respects and should not be interpreted limitedly.

Claims (14)

  1. ์ง€๋ฐ˜์— ์ˆ˜์ง์œผ๋กœ ๊ตด์ฐฉ๋œ ๊ฒฝ์‚ฌ๊ด€์— ์‚ฝ์ž…๋˜์–ด ๊ทธ ๊ธธ์ด๋ฐฉํ–ฅ์œผ๋กœ ์ด๋™ ๊ฐ€๋Šฅํ•˜๋ฉฐ, ๊ฒฝ์‚ฌ๊ด€ ๋‚ด๋ฉด์˜ ๋ณ€์œ„๋ฅผ ์ ‘์ด‰์‹์œผ๋กœ ๊ฐ์ง€ํ•˜๋Š” ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜๋กœ์„œ, It is inserted into the inclined tube excavated perpendicularly to the ground and is movable in the longitudinal direction, and is a ground displacement measuring device that detects the displacement of the inner surface of the inclined tube by contact,
    ๊ฒฝ์‚ฌ๊ด€ ๋‚ด์—์„œ ๊ทธ ๊ธธ์ด๋ฐฉํ–ฅ์œผ๋กœ ์ด๋™์‹œ ์ธก์ • ํƒ€์ด๋ฐ๋งˆ๋‹ค 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„๋ฅผ ์ธก์ •ํ•˜๋Š” ์„ผ์‹ฑ์ˆ˜๋‹จ;Sensing means for measuring a three-dimensional coordinate displacement at every measurement timing when moving in the longitudinal direction of the inclined tube;
    ์ƒ๊ธฐ ์ธก์ • ํƒ€์ด๋ฐ์„ ์„ค์ •ํ•˜๋Š” ํƒ€์ด๋ฐ์„ค์ •์ˆ˜๋‹จ;Timing setting means for setting the measurement timing;
    ์ƒ๊ธฐ ์„ผ์‹ฑ์ˆ˜๋‹จ์—์„œ ์ธก์ •ํ•œ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„ ๋ฐ์ดํ„ฐ๋ฅผ ์ง€๋ฐ˜๋ณ€์œ„๋Ÿ‰์œผ๋กœ ์—ฐ์‚ฐํ•˜๋Š” ๋ณ€์œ„๋Ÿ‰์—ฐ์‚ฐ์ˆ˜๋‹จ;Displacement amount calculation means for calculating three-dimensional coordinate displacement data measured by the sensing means as ground displacement;
    ์„ ํฌํ•จํ•˜์—ฌ ๊ตฌ์„ฑ๋œ ๊ฒƒ์„ ํŠน์ง•์œผ๋กœ ํ•˜๋Š” ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜. Ground displacement measuring device comprising a.
  2. ์ œ1ํ•ญ์— ์žˆ์–ด์„œ, The method of claim 1,
    ์ƒ๊ธฐ ์„ผ์‹ฑ์ˆ˜๋‹จ์€ 3์ถ• ์Ÿˆ์ด๋กœ์„ผ์„œ ๋˜๋Š” 3์ถ• ๊ฐ€์†๋„์„ผ์„œ ์ค‘์˜ ์–ด๋Š ํ•˜๋‚˜์ธ ๊ฒƒ์„ ํŠน์ง•์œผ๋กœ ํ•˜๋Š” ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜. The sensing means is ground displacement measuring device, characterized in that any one of a three-axis gyro sensor or three-axis acceleration sensor.
  3. ์ œ1ํ•ญ์— ์žˆ์–ด์„œ, The method of claim 1,
    ์ƒ๊ธฐ ์„ผ์‹ฑ์ˆ˜๋‹จ์€ 2์ถ• ์Ÿˆ์ด๋กœ์„ผ์„œ ๋˜๋Š” 2์ถ• ๊ฐ€์†๋„์„ผ์„œ ์ค‘์˜ ์–ด๋Š ํ•˜๋‚˜์™€ ์ง€๋ฐ˜ ์ˆ˜์ง๋ฐฉํ–ฅ ์ด๋™๊ฑฐ๋ฆฌ ์ธก์ •์„ผ์„œ์˜ ์กฐํ•ฉ์œผ๋กœ ์ด๋ค„์ง„ ๊ฒƒ์„ ํŠน์ง•์œผ๋กœ ํ•˜๋Š” ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜. The sensing means is ground displacement measuring device characterized in that the combination of any one of the two-axis gyro sensor or two-axis acceleration sensor and the vertical movement distance measurement sensor in the ground.
  4. ์ œ1ํ•ญ์— ์žˆ์–ด์„œ, The method of claim 1,
    ์ƒ๊ธฐ ์„ผ์‹ฑ์ˆ˜๋‹จ์€ ์ƒํ˜ธ ๋…๋ฆฝ์ ์ธ ์ธก์ •๋ฐฉ์‹์„ ๊ฐ–๋Š” ๋ณต์ˆ˜์˜ ์„ผ์‹ฑ์ˆ˜๋‹จ์œผ๋กœ ๊ตฌ์„ฑ๋˜๋ฉฐ, ์ƒ๊ธฐ ๊ฐ ์„ผ์‹ฑ์ˆ˜๋‹จ์ด ์ธก์ •ํ•œ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„ ๋ฐ์ดํ„ฐ๋ฅผ ์ƒํ˜ธ ๋น„๊ตํ•˜์—ฌ ๋ณด์ •ํ•˜๋Š” ๊ธฐ๋Šฅ์„ ๊ตฌ๋น„ํ•œ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜.The sensing means is composed of a plurality of sensing means having a mutually independent measurement method, the ground displacement measuring apparatus having a function to compare and correct the three-dimensional coordinate displacement data measured by each sensing means.
  5. ์ œ4ํ•ญ์— ์žˆ์–ด์„œ, The method of claim 4, wherein
    ์ƒ๊ธฐ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„ ๋ฐ์ดํ„ฐ์˜ ์ƒํ˜ธ ๋น„๊ต ๋ฐ ๋ณด์ •์€, The mutual comparison and correction of the three-dimensional coordinate displacement data,
    ์ผ์ธก ์„ผ์‹ฑ์ˆ˜๋‹จ์ด ์ธก์ •ํ•œ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„ ๋ฐ์ดํ„ฐ๋ฅผ ๊ธฐ์ค€์œผ๋กœ, ํƒ€์ธก ์„ผ์‹ฑ์ˆ˜๋‹จ์ด ์ธก์ •ํ•œ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„ ๋ฐ์ดํ„ฐ ์ค‘ ๊ธฐ์„ค์ •๋œ ์˜ค์ฐจ๋ฒ”์œ„๋ฅผ ๋„˜์–ด์„œ๋Š” ๊ฐ’์„ ๋‚˜ํƒ€๋‚ธ ๊ฒฝ์šฐ๋ฅผ ์—๋Ÿฌ๋กœ ํŒ๋‹จํ•˜์—ฌ ์ฒ˜๋ฆฌํ•˜๋„๋ก ๊ตฌ์„ฑ๋œ ๊ฒƒ์„ ํŠน์ง•์œผ๋กœ ํ•˜๋Š” ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜. Based on the three-dimensional coordinate displacement data measured by one sensing means, the ground characterized in that it is configured to determine if the value that exceeds the predetermined error range of the three-dimensional coordinate displacement data measured by the other sensing means to process as an error. Displacement measuring device.
  6. ์ œ5ํ•ญ์— ์žˆ์–ด์„œ, The method of claim 5,
    ์ƒ๊ธฐ ๋ณต์ˆ˜์˜ ์„ผ์‹ฑ์ˆ˜๋‹จ์€ ์ ์–ด๋„ 2๊ฐœ์˜ ์„ผ์„œ๋กœ ๊ตฌ์„ฑ๋˜๋ฉฐ, 3์ถ• ์Ÿˆ์ด๋กœ์„ผ์„œ์™€ 3์ถ• ๊ฐ€์†๋„์„ผ์„œ๋ฅผ ํฌํ•จํ•œ ๊ฒƒ์„ ํŠน์ง•์œผ๋กœ ํ•˜๋Š” ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜. The plurality of sensing means is composed of at least two sensors, ground displacement measuring apparatus comprising a three-axis gyro sensor and a three-axis acceleration sensor.
  7. ์ œ5ํ•ญ์— ์žˆ์–ด์„œ, The method of claim 5,
    ์ƒ๊ธฐ ๋ณต์ˆ˜์˜ ์„ผ์‹ฑ์ˆ˜๋‹จ์€ ์ ์–ด๋„ 2๊ฐœ์˜ ์„ผ์„œ ์กฐํ•ฉ์œผ๋กœ ๊ตฌ์„ฑ๋˜๋ฉฐ, The plurality of sensing means is composed of at least two sensor combinations,
    ์ƒ๊ธฐ ์„ผ์„œ ์กฐํ•ฉ์€ 2์ถ• ์Ÿˆ์ด๋กœ์„ผ์„œ์™€ ์ง€๋ฐ˜ ์ˆ˜์ง๋ฐฉํ–ฅ ์ด๋™๊ฑฐ๋ฆฌ ์ธก์ •์„ผ์„œ์˜ ์กฐํ•ฉ๊ณผ 2์ถ• ๊ฐ€์†๋„์„ผ์„œ์™€ ์ง€๋ฐ˜ ์ˆ˜์ง๋ฐฉํ–ฅ ์ด๋™๊ฑฐ๋ฆฌ ์ธก์ •์„ผ์„œ์˜ ์กฐํ•ฉ์„ ํฌํ•จํ•œ ๊ฒƒ์„ ํŠน์ง•์œผ๋กœ ํ•˜๋Š” ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜. The sensor combination is a ground displacement measuring apparatus comprising a combination of a two-axis gyro sensor and a ground vertical movement distance measuring sensor and a combination of a two-axis acceleration sensor and a ground vertical movement distance measuring sensor.
  8. ์ œ1ํ•ญ ๋˜๋Š” ์ œ2ํ•ญ, ์ œ4ํ•ญ, ์ œ5ํ•ญ, ์ œ6ํ•ญ ์ค‘์˜ ์–ด๋Š ํ•œ ํ•ญ์— ์žˆ์–ด์„œ, The method according to any one of claims 1 or 2, 4, 5, and 6,
    ์ง€๋ฐ˜ ์ˆ˜์ง๋ฐฉํ–ฅ ์ด๋™๊ฑฐ๋ฆฌ ์ธก์ •์„ผ์„œ ๋˜๋Š” ์˜จ๋„์„ผ์„œ ์ค‘์˜ ์ ์–ด๋„ ์–ด๋Š ํ•˜๋‚˜๋ฅผ ๋ณด์กฐ ์„ผ์‹ฑ์ˆ˜๋‹จ์œผ๋กœ ๋” ๊ตฌ๋น„ํ•˜์—ฌ, ์ƒ๊ธฐ ์„ผ์‹ฑ์ˆ˜๋‹จ์ด ์ธก์ •ํ•œ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„ ๋ฐ์ดํ„ฐ๋ฅผ ๋ณด์ •ํ•˜๋Š” ๊ธฐ๋Šฅ์„ ๊ตฌ๋น„ํ•œ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜.A ground displacement measuring apparatus further comprising at least one of a ground vertical movement distance measuring sensor and a temperature sensor as an auxiliary sensing means to correct three-dimensional coordinate displacement data measured by the sensing means.
  9. ์ œ1ํ•ญ ๋‚ด์ง€ ์ œ7ํ•ญ ์ค‘์˜ ์–ด๋Š ํ•œ ํ•ญ์— ์žˆ์–ด์„œ, The method according to any one of claims 1 to 7,
    ์ƒ๊ธฐ ํƒ€์ด๋ฐ์„ค์ •์ˆ˜๋‹จ์€ ์ƒํ˜ธ ๋…๋ฆฝ์ ์ธ ๋ณต์ˆ˜์˜ ์ฃผํŒŒ์ˆ˜๋ฅผ ์ธก์ • ํƒ€์ด๋ฐ์œผ๋กœ ์„ค์ •ํ•  ์ˆ˜ ์žˆ๋„๋ก ๊ตฌ๋น„๋˜์–ด, ๊ฐ ์ฃผํŒŒ์ˆ˜๋ณ„๋กœ ์ƒ๊ธฐ ์„ผ์‹ฑ์ˆ˜๋‹จ์ด ์ธก์ •ํ•œ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„ ๋ฐ์ดํ„ฐ๋ฅผ ์ƒํ˜ธ ๋น„๊ตํ•˜์—ฌ ๋ณด์ •ํ•˜๋Š” ๊ธฐ๋Šฅ์„ ๊ตฌ๋น„ํ•œ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜.The timing setting means is provided so as to set a plurality of mutually independent frequencies as the measurement timing, the ground displacement measuring apparatus having a function of comparing and correcting the three-dimensional coordinate displacement data measured by the sensing means for each frequency.
  10. ์ œ9ํ•ญ์— ์žˆ์–ด์„œ, The method of claim 9,
    ์ƒ๊ธฐ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„ ๋ฐ์ดํ„ฐ์˜ ์ƒํ˜ธ ๋น„๊ต ๋ฐ ๋ณด์ •์€, The mutual comparison and correction of the three-dimensional coordinate displacement data,
    ํ•˜๋‚˜์˜ ์ฃผํŒŒ์ˆ˜๋ฅผ ์ธก์ • ํƒ€์ด๋ฐ์œผ๋กœ ์„ค์ •ํ•˜์—ฌ ์ธก์ •ํ•œ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„ ๋ฐ์ดํ„ฐ๋ฅผ ๊ธฐ์ค€์œผ๋กœ, ๋˜๋‹ค๋ฅธ ์ฃผํŒŒ์ˆ˜๋ฅผ ์ธก์ • ํƒ€์ด๋ฐ์œผ๋กœ ์„ค์ •ํ•˜์—ฌ ์ธก์ •ํ•œ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„ ๋ฐ์ดํ„ฐ ์ค‘ ๊ธฐ์„ค์ •๋œ ์˜ค์ฐจ๋ฒ”์œ„๋ฅผ ๋„˜์–ด์„œ๋Š” ๊ฐ’์„ ๋‚˜ํƒ€๋‚ธ ๊ฒฝ์šฐ๋ฅผ ์—๋Ÿฌ๋กœ ํŒ๋‹จํ•˜์—ฌ ์ฒ˜๋ฆฌํ•˜๋„๋ก ๊ตฌ์„ฑ๋œ ๊ฒƒ์„ ํŠน์ง•์œผ๋กœ ํ•˜๋Š” ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜.Based on the three-dimensional coordinate displacement data measured by setting one frequency as the measurement timing, and displaying a value exceeding the preset error range among the three-dimensional coordinate displacement data measured by setting another frequency as the measurement timing. Ground displacement measuring apparatus, characterized in that configured to determine and process.
  11. ์ œ10ํ•ญ์— ์žˆ์–ด์„œ, The method of claim 10,
    ์ง€๋ฐ˜ ์ˆ˜์ง๋ฐฉํ–ฅ ์ด๋™๊ฑฐ๋ฆฌ ์ธก์ •์„ผ์„œ ๋˜๋Š” ์˜จ๋„์„ผ์„œ ์ค‘์˜ ์ ์–ด๋„ ์–ด๋Š ํ•˜๋‚˜๋ฅผ ๋ณด์กฐ ์„ผ์‹ฑ์ˆ˜๋‹จ์œผ๋กœ ๋” ๊ตฌ๋น„ํ•˜์—ฌ, ์ƒ๊ธฐ ์„ผ์‹ฑ์ˆ˜๋‹จ์ด ์ธก์ •ํ•œ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„ ๋ฐ์ดํ„ฐ๋ฅผ ๋ณด์ •ํ•˜๋Š” ๊ธฐ๋Šฅ์„ ๊ตฌ๋น„ํ•œ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜.A ground displacement measuring apparatus further comprising at least one of a ground vertical movement distance measuring sensor and a temperature sensor as an auxiliary sensing means to correct three-dimensional coordinate displacement data measured by the sensing means.
  12. ์ œ1ํ•ญ ๋‚ด์ง€ ์ œ7ํ•ญ ์ค‘์˜ ์–ด๋Š ํ•œ ํ•ญ์— ์žˆ์–ด์„œ, The method according to any one of claims 1 to 7,
    ์ƒ๊ธฐ ์„ผ์‹ฑ์ˆ˜๋‹จ์€ ๋ณต์ˆ˜์˜ ์„ผ์‹ฑ์ˆ˜๋‹จ์œผ๋กœ ๊ตฌ์„ฑ๋˜๋ฉฐ, The sensing means is composed of a plurality of sensing means,
    ์ƒ๊ธฐ ํƒ€์ด๋ฐ์„ค์ •์ˆ˜๋‹จ์€ ๊ฐ ์„ผ์‹ฑ์ˆ˜๋‹จ๋ณ„๋กœ ์ƒํ˜ธ ๋…๋ฆฝ์ ์ธ ๋ณต์ˆ˜์˜ ์ฃผํŒŒ์ˆ˜๋ฅผ ์ธก์ • ํƒ€์ด๋ฐ์œผ๋กœ ์„ค์ •ํ•  ์ˆ˜ ์žˆ๋„๋ก ๊ตฌ๋น„๋˜์–ด, The timing setting means is provided to set a plurality of frequencies independent of each sensing means as the measurement timing,
    ์ƒ๊ธฐ ๊ฐ ์„ผ์‹ฑ์ˆ˜๋‹จ์ด ์ธก์ •ํ•œ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„ ๋ฐ์ดํ„ฐ๋ฅผ ์ƒํ˜ธ ๋น„๊ตํ•˜์—ฌ ๋ณด์ •ํ•˜๋Š” ๊ธฐ๋Šฅ์„ ๊ตฌ๋น„ํ•œ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜.And a ground displacement measuring device having a function of comparing and correcting three-dimensional coordinate displacement data measured by the sensing means.
  13. ์ œ12ํ•ญ์— ์žˆ์–ด์„œ, The method of claim 12,
    ์ƒ๊ธฐ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„ ๋ฐ์ดํ„ฐ์˜ ์ƒํ˜ธ ๋น„๊ต ๋ฐ ๋ณด์ •์€, The mutual comparison and correction of the three-dimensional coordinate displacement data,
    ํ•˜๋‚˜์˜ ์ฃผํŒŒ์ˆ˜๋ฅผ ์ธก์ • ํƒ€์ด๋ฐ์œผ๋กœ ์„ค์ •ํ•˜์—ฌ ์ธก์ •ํ•œ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„ ๋ฐ์ดํ„ฐ๋ฅผ ๊ธฐ์ค€์œผ๋กœ, ๋˜๋‹ค๋ฅธ ์ฃผํŒŒ์ˆ˜๋ฅผ ์ธก์ • ํƒ€์ด๋ฐ์œผ๋กœ ์„ค์ •ํ•˜์—ฌ ์ธก์ •ํ•œ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„ ๋ฐ์ดํ„ฐ ์ค‘ ๊ธฐ์„ค์ •๋œ ์˜ค์ฐจ๋ฒ”์œ„๋ฅผ ๋„˜์–ด์„œ๋Š” ๊ฐ’์„ ๋‚˜ํƒ€๋‚ธ ๊ฒฝ์šฐ๋ฅผ ์—๋Ÿฌ๋กœ ํŒ๋‹จํ•˜์—ฌ ์ฒ˜๋ฆฌํ•˜๋„๋ก ๊ตฌ์„ฑ๋œ ๊ฒƒ์„ ํŠน์ง•์œผ๋กœ ํ•˜๋Š” ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜.Based on the three-dimensional coordinate displacement data measured by setting one frequency as the measurement timing, and displaying a value exceeding the preset error range among the three-dimensional coordinate displacement data measured by setting another frequency as the measurement timing. Ground displacement measuring apparatus, characterized in that configured to determine and process.
  14. ์ œ13ํ•ญ์— ์žˆ์–ด์„œ, The method of claim 13,
    ์ง€๋ฐ˜ ์ˆ˜์ง๋ฐฉํ–ฅ ์ด๋™๊ฑฐ๋ฆฌ ์ธก์ •์„ผ์„œ ๋˜๋Š” ์˜จ๋„์„ผ์„œ ์ค‘์˜ ์ ์–ด๋„ ์–ด๋Š ํ•˜๋‚˜๋ฅผ ๋ณด์กฐ ์„ผ์‹ฑ์ˆ˜๋‹จ์œผ๋กœ ๋” ๊ตฌ๋น„ํ•˜์—ฌ, ์ƒ๊ธฐ ์„ผ์‹ฑ์ˆ˜๋‹จ์ด ์ธก์ •ํ•œ 3์ฐจ์› ์ขŒํ‘œ ๋ณ€์œ„ ๋ฐ์ดํ„ฐ๋ฅผ ๋ณด์ •ํ•˜๋Š” ๊ธฐ๋Šฅ์„ ๊ตฌ๋น„ํ•œ ์ง€๋ฐ˜๋ณ€์œ„ ์ธก์ •์žฅ์น˜.A ground displacement measuring apparatus further comprising at least one of a ground vertical movement distance measuring sensor and a temperature sensor as an auxiliary sensing means to correct three-dimensional coordinate displacement data measured by the sensing means.
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Publication number Priority date Publication date Assignee Title
CN103940401A (en) * 2014-04-30 2014-07-23 ไธœๅŒ—ๅคงๅญฆ Gas bearing shale absorption strain testing device and method under confining pressure bias pressure constant temperature environment
CN116067333A (en) * 2023-03-14 2023-05-05 ๅฑฑไธœ็œ็‰ฉๅŒ–ๆŽขๅ‹˜ๆŸฅ้™ข Method and system for determining deformation of foundation pit support pile by adopting comprehensive theory

Families Citing this family (7)

* Cited by examiner, โ€  Cited by third party
Publication number Priority date Publication date Assignee Title
KR101310999B1 (en) * 2011-12-30 2013-09-24 ๊ฒฝ์„ฑ๋Œ€ํ•™๊ต ์‚ฐํ•™ํ˜‘๋ ฅ๋‹จ Apparatus for inspecting surface of hole in rock
CN105783823B (en) * 2016-05-10 2018-10-30 ไบ‘ๅ—็œไบค้€š่ง„ๅˆ’่ฎพ่ฎก็ ”็ฉถ้™ข Multinode overlength deep soils device and monitoring method
KR101876451B1 (en) * 2016-08-22 2018-07-11 ์ด๋ฏผํฌ Control apparatus for inspecting surface of hole in rock
JP7261439B2 (en) * 2018-10-16 2023-04-20 ๆ ชๅผไผš็คพๅผ˜ๆ „ใƒ‰ใƒชใƒผใƒ ใƒฏใƒผใ‚ฏใ‚น Pipe measurement system, pipe measurement device, information processing device and program
JP7290885B2 (en) * 2018-10-16 2023-06-14 ๆ ชๅผไผš็คพๅผ˜ๆ „ใƒ‰ใƒชใƒผใƒ ใƒฏใƒผใ‚ฏใ‚น Piping measuring device
CN112033317B (en) * 2020-09-02 2022-04-22 ไธญ็…ค็ง‘ๅทฅ้›†ๅ›ข่ฅฟๅฎ‰็ ”็ฉถ้™ขๆœ‰้™ๅ…ฌๅธ Method for online measurement of three-dimensional data of escape hole of manned lifting cabin
KR102441473B1 (en) * 2021-04-08 2022-09-06 ์ง€์›์„ญ Pipe-roof inspection device and the inspection method using the device

Citations (4)

* Cited by examiner, โ€  Cited by third party
Publication number Priority date Publication date Assignee Title
JP2003232631A (en) * 2002-02-08 2003-08-22 Tobishima Corp Ground deformation measuring system with optical fiber sensor
KR100416197B1 (en) * 1998-02-17 2004-01-31 ๋„์‹œ๋ฐ” ์—”์ง€๋‹ˆ์–ด๋ง ๊ฐ€๋ถ€์‹œ๋ผ๊ฐ€์ด์ƒค Geographical displacement sensing unit and monitoring apparatus using the same
KR100456485B1 (en) * 2004-02-11 2004-11-10 (์ฃผ)์ง€์— ์ง€ A transformation survey method and apparatus of the underground
KR100708781B1 (en) * 2005-08-09 2007-04-18 ์ฃผ์‹ํšŒ์‚ฌ ๋กœํ…์ธ์ŠคํŠธ๋ฃจ๋จผํŠธ Apparatus for Measuring Displacement of Engineering Structure and Underground Displacement

Family Cites Families (12)

* Cited by examiner, โ€  Cited by third party
Publication number Priority date Publication date Assignee Title
AU533909B2 (en) * 1980-10-23 1983-12-15 Sundstrand Data Control, Inc. Bore-hole survey apparatus
JPH03251717A (en) * 1990-03-01 1991-11-11 Shimizu Corp Method and apparatus for measuring subsidence for construction
JP3143204B2 (en) * 1991-11-11 2001-03-07 ไธ‰่ฑใƒ—ใƒฌใ‚ทใ‚ธใƒงใƒณๆ ชๅผไผš็คพ Hole bending measuring device and hole bending measuring method
JP3339731B2 (en) * 1993-06-29 2002-10-28 ไธ‰่ฑใƒ—ใƒฌใ‚ทใ‚ธใƒงใƒณๆ ชๅผไผš็คพ Hole bending measurement method
JPH07128058A (en) * 1993-11-04 1995-05-19 Hitachi Cable Ltd Method for measuring conduit
JPH08178653A (en) * 1994-12-27 1996-07-12 Hitachi Cable Ltd Embedded pipe line position measuring system
JPH09189548A (en) * 1996-01-09 1997-07-22 East Japan Railway Co Attitude angle sensor for train
SE509530C2 (en) * 1997-04-01 1999-02-08 Spectra Precision Ab Surveying method and surveying apparatus comprising a radio navigation unit
JPH1114356A (en) * 1997-06-23 1999-01-22 Raito Kogyo Co Ltd Three-dimensional position detecting method
JP2001343396A (en) * 2000-06-02 2001-12-14 Japan Aviation Electronics Industry Ltd Sensor diagnostic device
JP4013820B2 (en) * 2003-04-30 2007-11-28 ๏ผช๏ฝ†๏ฝ…ใ‚จใƒณใ‚ธใƒ‹ใ‚ขใƒชใƒณใ‚ฐๆ ชๅผไผš็คพ Pipeline shape measurement evaluation method
JP4591328B2 (en) * 2005-11-18 2010-12-01 ๆ ชๅผไผš็คพใƒ‡ใƒณใ‚ฝใƒผ Vehicle running state detection device, navigation device, and program

Patent Citations (4)

* Cited by examiner, โ€  Cited by third party
Publication number Priority date Publication date Assignee Title
KR100416197B1 (en) * 1998-02-17 2004-01-31 ๋„์‹œ๋ฐ” ์—”์ง€๋‹ˆ์–ด๋ง ๊ฐ€๋ถ€์‹œ๋ผ๊ฐ€์ด์ƒค Geographical displacement sensing unit and monitoring apparatus using the same
JP2003232631A (en) * 2002-02-08 2003-08-22 Tobishima Corp Ground deformation measuring system with optical fiber sensor
KR100456485B1 (en) * 2004-02-11 2004-11-10 (์ฃผ)์ง€์— ์ง€ A transformation survey method and apparatus of the underground
KR100708781B1 (en) * 2005-08-09 2007-04-18 ์ฃผ์‹ํšŒ์‚ฌ ๋กœํ…์ธ์ŠคํŠธ๋ฃจ๋จผํŠธ Apparatus for Measuring Displacement of Engineering Structure and Underground Displacement

Cited By (2)

* Cited by examiner, โ€  Cited by third party
Publication number Priority date Publication date Assignee Title
CN103940401A (en) * 2014-04-30 2014-07-23 ไธœๅŒ—ๅคงๅญฆ Gas bearing shale absorption strain testing device and method under confining pressure bias pressure constant temperature environment
CN116067333A (en) * 2023-03-14 2023-05-05 ๅฑฑไธœ็œ็‰ฉๅŒ–ๆŽขๅ‹˜ๆŸฅ้™ข Method and system for determining deformation of foundation pit support pile by adopting comprehensive theory

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