CN201590481U - Mobile antenna device - Google Patents
Mobile antenna device Download PDFInfo
- Publication number
- CN201590481U CN201590481U CN2010201128438U CN201020112843U CN201590481U CN 201590481 U CN201590481 U CN 201590481U CN 2010201128438 U CN2010201128438 U CN 2010201128438U CN 201020112843 U CN201020112843 U CN 201020112843U CN 201590481 U CN201590481 U CN 201590481U
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- antenna
- master controller
- support
- gyroscope
- angle
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Abstract
The utility model discloses a mobile antenna device. The mobile antenna device comprises a base, a stand, an antenna, a main controller, a GPS location system, a compass, a step motor and a gyro, wherein the stand, the antenna, the main controller, the GPS location system, the compass, the step motor and the gyro are arranged on the base; the stand is rotatably arranged on the base; the antenna is fixed on the stand; the control end of the step motor is connected with the stand to adjust the position of the stand under the control of the main controller; the GPS location system, the compass and the gyro are connected with the main controller for transmitting the detected geographic coordinate, the deviation angle and the angle change value of the current position to the main controller. The antenna structure can intelligently change the elevation angle and the azimuth angle of the antenna during the advancing of ships and vehicles to ensure that the antenna faces the position with satellite signals all the time, thereby ensuring the signal receiving strength.
Description
Technical field
The utility model belongs to the communications field, is meant especially a kind ofly to be applied on the car and boat and mobile antenna apparatus that received signal is good.
Background technology
Along with the development of vehicle-mounted technology, the amusement function of vehicle is more and more, has enriched people's the life of travelling, yet, on car and boat, still there are some amusement functions to realize, as watch satellite programming.As everyone knows, when watching satellite programming, wired usually and wireless dual mode when using wired mode, needs a cable television line, carries out the conduction of signal, and we know that it is impracticable therefore using wired mode because car and boat often move everywhere; And for wireless mode, antenna alignment need be sent the direction of this satellite programming, be in the time spent, need artificial constantly rotary antenna, until can receiving the reasonable program of effect, yet, because car and boat are constantly to move, and therefore the antenna operated by rotary motion can't remove rotary antenna by manpower on the top of car and boat.
In view of this, the design people studies improvement at the shortcoming that can't watch satellite programming on the mobile traffics such as present car and boat at antenna structure, and this case produces thus.
The utility model content
Main purpose of the present utility model is to provide a kind of mobile antenna apparatus, its can be in the car and boat traveling process intelligence change the elevation angle and the azimuth of antenna, make antenna all the time towards the position of satellite-signal, guarantee the intensity of received signal.
In order to reach above-mentioned purpose, solution of the present utility model is:
A kind of mobile antenna apparatus, comprise base and be located at support, antenna, master controller, GPS navigation system, compass, stepping motor, gyroscope on the base, support is arranged on the base rotationally, antenna is fixed on the support, the Stepping Motor Control end is connected with support, adjusts the position of support under the control of master controller; GPS navigation system, compass and gyroscope all are connected with master controller, and detected current location longitude and latitude, the deviation angle and angle changing value are sent into master controller.
Above-mentioned stepping motor comprises elevation angle stepping motor and azimuth stepping motor, all is connected with master controller, and adjusts the rotation elevation angle and the azimuth of support under the control of master controller.
Above-mentioned gyroscope comprises azimuth gyroscope, elevation angle gyroscope and roll angle gyroscope, all is connected with master controller, and azimuth, the elevation angle and the roll angle value of the support that records are sent into master controller.
Above-mentioned antenna is a plate aerial.
After adopting such scheme, the utlity model has following improvement:
(1) set in advance positional information at corresponding each satellite programming of each longitude and latitude, then antenna is adjusted to correspondence position, make it accurately send the position towards signal, thereby the satellite-signal that receives is the strongest, effect is best;
(2) GPS navigation system and compass are issued master controller with the current longitude and latitude and the deviation angle in real time, and master controller can be adjusted the location status of antenna as required in real time, guarantee that it receives stronger satellite-signal all the time, guarantees result of use;
(3) all components is all organized and is located on the base, and is whole mobile very convenient, and can be installed in the top of car and boat fast, easy to use.
Description of drawings
Fig. 1 is a structured flowchart of the present utility model;
Fig. 2 is a course of work schematic diagram of the present utility model;
Fig. 3 to Fig. 9 is that antenna carries out the schematic diagram that all angles are rotated.
Embodiment
Below in conjunction with drawings and the specific embodiments the concrete composition of the present utility model and the course of work are elaborated.
With reference to shown in Figure 1, the utility model provides a kind of mobile antenna apparatus, comprise antenna 1 (using plate aerial among this embodiment), master controller 2, GPS navigation system 3, stepping motor 4, base 5, support 6, gyroscope 7 and compass 8, this kind antenna assembly is by the satellite-signal positional information of at first default corresponding each longitude and latitude, each satellite programming, and in the car and boat traveling process control antenna 1 all the time towards this satellite-signal, thereby guarantee the excellent reception signal strength signal intensity, make car and boat also can watch satellite programming in the process of moving.
Stepping motor 4 comprises elevation angle stepping motor 41 and azimuth stepping motor 42, its control end all connects support 6, under the control of master controller 2, regulate the rotation direction and the angle of support 6, realize the comprehensive rotation of antenna 1, can receive satellite-signal clearly all the time to guarantee antenna 1.
Store the positional information of the signal of corresponding each frequency range in the master controller 2, because each satellite programming and frequency range are to concern one to one, as long as therefore know the required satellite programming of watching, can find the positional information of its signal, and may command support 6 turns to towards this position, and the signal strength signal intensity that antenna 1 is received is the strongest.
Below in conjunction with Fig. 2 the concrete course of work of the present utility model is done an explanation.
(1) at first carries out the initialization of system, comprise the software in the master controller 2 and the initialization of antenna 1, make antenna 1 be in initial position;
(2) GPS navigation system 3, compass 9 detect the longitude and latitude and the deviation angle information of current location, and send in the master controller 2;
(3) master controller 2 is according to the frequency range of the satellite programming that will watch, read its positional information (because the frequency range of each satellite programming is unique at current longitude and latitude, therefore determine that frequency range is this program of lockable), and according to deviation angle calculated difference, be scaled the step number of advancing of stepping motor 4, control elevation angle stepping motor 41 and azimuth stepping motor 42 are adjusted into the relevant position with support 6, can be with reference to figure 3 to shown in Figure 9, be illustrated under the control of master controller 2, support 6 carries out the schematic diagram of level and vertical direction rotation;
(4) be in course of adjustment, antenna 1 is the power of detection signal strength simultaneously, and send in the master controller 2, specifically can be with reference to shown in Figure 1, the satellite-signal that antenna 1 is received carries out synthesizing with power supply signal after the power division, behind low noise amplification, intermediate frequency filtering, low noise amplification, signal amplification demodulator, send into master controller 2 successively then, judge whether to have entered the signal area by master controller 2 according to strong and weak situation, if entered the signal area, change step (5) over to, if also do not enter, then change step (7);
(5) azimuth gyroscope 71, elevation angle gyroscope 72 and roll angle gyroscope 73 regularly detect azimuth, the elevation angle and the roll angle of antenna 1, and send into master controller 2, and master controller 2 is scaled the step number of advancing of stepping motor 4 according to the various angle values that receive;
(6) master controller 2 reads the signal strength signal intensity that antenna 1 receives simultaneously, and judge whether signal is lost, if lose the longitude and latitude and the deviation angle that then reads antenna 1 current location again, repeating step (2), do not continue then to judge whether signal strength signal intensity needs to proofread and correct, and need not proofread and correct the current state of then keeping antenna 1, proofreaies and correct if need if lose, then master controller 2 reads the angle value of gyroscope 7 again, repeating step (5);
(7) master controller 2 control step motors 4 carry out the deflection diffusion mode, whether the also real-time twice detectability bit switch of each stepping triggers, if having triggered then reset current elevation value and azimuth value is default value, again the step number of advancing of stepping motor 4 then converts, repeating step (3), if limit switch does not trigger then master controller 2 control step motors 4 and support 6 is adjusted to assigned address, repeating step (4).
Above embodiment only is explanation technological thought of the present utility model; can not limit protection range of the present utility model with this; every according to the technological thought that the utility model proposes, any change of being done on the technical scheme basis all falls within the utility model protection range.
Claims (4)
1. mobile antenna apparatus, it is characterized in that: comprise base and be located at support, antenna, master controller, GPS navigation system, compass, stepping motor, gyroscope on the base, support is arranged on the base rotationally, antenna is fixed on the support, the Stepping Motor Control end is connected with support, adjusts the position of support under the control of master controller; GPS navigation system, compass and gyroscope all are connected with master controller, and detected current location longitude and latitude, the deviation angle and angle changing value are sent into master controller.
2. a kind of mobile antenna apparatus as claimed in claim 1 is characterized in that: described stepping motor comprises elevation angle stepping motor and azimuth stepping motor, all is connected with master controller, and adjusts the rotation elevation angle and the azimuth of support under the control of master controller.
3. a kind of mobile antenna apparatus as claimed in claim 1, it is characterized in that: described gyroscope comprises azimuth gyroscope, elevation angle gyroscope and roll angle gyroscope, all be connected, and azimuth, the elevation angle and the roll angle value of the support that records are sent into master controller with master controller.
4. a kind of mobile antenna apparatus as claimed in claim 1 is characterized in that: described antenna is a plate aerial.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2010201128438U CN201590481U (en) | 2010-02-01 | 2010-02-01 | Mobile antenna device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2010201128438U CN201590481U (en) | 2010-02-01 | 2010-02-01 | Mobile antenna device |
Publications (1)
Publication Number | Publication Date |
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CN201590481U true CN201590481U (en) | 2010-09-22 |
Family
ID=42750273
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN2010201128438U Expired - Fee Related CN201590481U (en) | 2010-02-01 | 2010-02-01 | Mobile antenna device |
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Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103458200A (en) * | 2012-05-30 | 2013-12-18 | 深圳感臻科技有限公司 | Novel star finder |
CN103594797A (en) * | 2013-11-28 | 2014-02-19 | 珠海迈越信息技术有限公司 | Satellite tracking system and method for satellite antenna |
CN105119041A (en) * | 2015-09-20 | 2015-12-02 | 金华技物光电研究所有限公司 | Full scope directional antenna system |
CN106774433A (en) * | 2017-01-17 | 2017-05-31 | 北京小米移动软件有限公司 | No-manned machine distant control method and device |
-
2010
- 2010-02-01 CN CN2010201128438U patent/CN201590481U/en not_active Expired - Fee Related
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103458200A (en) * | 2012-05-30 | 2013-12-18 | 深圳感臻科技有限公司 | Novel star finder |
CN103458200B (en) * | 2012-05-30 | 2017-03-29 | 深圳感臻科技有限公司 | A kind of Novel star finder |
CN103594797A (en) * | 2013-11-28 | 2014-02-19 | 珠海迈越信息技术有限公司 | Satellite tracking system and method for satellite antenna |
CN105119041A (en) * | 2015-09-20 | 2015-12-02 | 金华技物光电研究所有限公司 | Full scope directional antenna system |
CN105119041B (en) * | 2015-09-20 | 2017-10-31 | 金华技物光电研究所有限公司 | Gamut beam aerial system |
CN106774433A (en) * | 2017-01-17 | 2017-05-31 | 北京小米移动软件有限公司 | No-manned machine distant control method and device |
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Legal Events
Date | Code | Title | Description |
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C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20100922 Termination date: 20130201 |
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CF01 | Termination of patent right due to non-payment of annual fee |