CN108319189B - A kind of more running fire target missile control systems - Google Patents
A kind of more running fire target missile control systems Download PDFInfo
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- CN108319189B CN108319189B CN201810011630.7A CN201810011630A CN108319189B CN 108319189 B CN108319189 B CN 108319189B CN 201810011630 A CN201810011630 A CN 201810011630A CN 108319189 B CN108319189 B CN 108319189B
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- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B19/00—Programme-control systems
- G05B19/02—Programme-control systems electric
- G05B19/04—Programme control other than numerical control, i.e. in sequence controllers or logic controllers
- G05B19/042—Programme control other than numerical control, i.e. in sequence controllers or logic controllers using digital processors
- G05B19/0423—Input/output
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- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B2219/00—Program-control systems
- G05B2219/20—Pc systems
- G05B2219/25—Pc structure of the system
- G05B2219/25257—Microcontroller
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Abstract
The invention discloses a kind of more running fire target missile control systems, including target missile flight subsystem and ground control subsystem；The target missile flight subsystem is mainly used for attitude angular rate signal, altitude signal and the GPS signal in three directions when real-time measurement target missile flight, rudder machine control signal is formed according to control law, target missile attitude stabilization is controlled, is climbed by the program of setting, Ding Gaoping flies and course position control；The ground control subsystem includes that the connected transmitting station and transmitter control station of emission control cable is covered by N, the transmitting station is for control signal needed for providing ground control subsystem, cooperate transmitter control station to complete transmitting docking test and emission control to target missile, has the N hair continuous emission control function of target missile；The present invention can be realized the emission control and test of more running fire target missiles, improve target missile for target ability, and it is small in size easy to carry.
Description
Technical field
The invention belongs to target missile emission control technical fields, more particularly, to a kind of more running fire target missile control systems.
Background technique
In order to examine every tactics index of guided missile, in flight test in range need target missile true to nature simulation led to attack
The feature of bullet, with the continuous improvement of the various abilities of guided missile, such as speed is fast, operational distance is remote, high lower bound range is big, Yi Jizuo
It fights the increasingly complex of environment, usually putting forward higher requirements for target ability to target missile,
Target missile is to provide target in the test for examining missile performance for guided missile and work as target for target task.Currently, training
Target for target task is essentially all single transmitting, and with the needs that actual combatization is drilled, it is quickly close can to develop a kind of simulation
The system for collecting target becomes urgent need.
Summary of the invention
Aiming at the above defects or improvement requirements of the prior art, the present invention provides a kind of more running fire target missile control systems,
The system makes transmitting station have more running fire target missile emission functions by carrying out program setting to transmitting station；Emitting
The signal regulating panel and emission interface to match with target missile number is set in console, conditioning parsing is carried out to received control instruction
After send emission interface, control target missile executes continuous transmitting movement, improve target missile for target ability.
To achieve the above object, according to one aspect of the present invention, a kind of more running fire target missile control systems are provided, including
Target missile flight subsystem and ground control subsystem；
Target missile flight subsystem be mainly used for the attitude angular rate signal in three directions when real-time measurement target missile flight,
Altitude signal and GPS signal form rudder machine control signal according to control law, target missile attitude stabilization are controlled, by the journey of setting
Sequence is climbed, Ding Gaoping flies and course position control；
Ground control subsystem includes that the connected transmitting station and transmitter control station of emission control cable, hair are covered by N
Station is penetrated for control signal needed for providing ground control subsystem, switches the transmission channel of different target missiles, cooperation transmitting
Console completes transmitting docking test and emission control to target missile, realizes that N sends out the continuous emission control function of target missile, wherein N is
Natural number；
Transmitter control station is used to receive the control signal of transmitting station, completes the emission control to target missile；Emission control
Platform includes N number of signal regulating panel, N number of test interface and N number of emission interface, and n-th target missile passes through test cable and transmitting respectively
Cable is connect with n-th test interface and n-th emission interface, and signal regulating panel carries out conditioning parsing to received control instruction
After be sent to test interface and emission interface, control corresponding target missile and execute transmitting movement.
Preferably, above-mentioned more running fire target missile control systems, transmitting station includes industrial personal computer, display and station,
Industrial personal computer includes controller, On-off signal board, output switch parameter board, serial ports board and AD/DA multi-functional data board,
Station includes switch, indicator light, keyboard and mouse, and display, keyboard and mouse constitute human-computer interaction interface, and operator is logical
The state in place that human-computer interaction interface obtains target missile is crossed, and passes through the transmission channel of switching difference target missile.
Preferably, above-mentioned more running fire target missile control systems, target missile flight subsystem include control cabinet, electrical cabin and
Rudder system, electrical cabin and rudder system are connected with control cabinet, and control cabinet and rudder system constitute target missile flight subsystem
Control unit, electrical cabin turn electric power supply control and priming system instruction output for target missile flight subsystem；
Its control cabinet includes Gyro, flight control computer, altimeter and bottom plate；Gyro, flight control computer and height
Degree table is connected with bottom plate, and bottom plate is equipped with electrical cabin connecting interface；
Electrical cabin includes telemetering electric plates, battery and telemetering radio station, and the working power of telemetering electric plates is provided by battery, electricity
Pond and telemetering radio station are connected with telemetering electric plates, and telemetering radio station is connected by telemetry interface with the bottom plate in control cabinet, to connect
Receive the target missile state parameter that flight control computer issues；
Rudder system includes that rudder puts plate and electric steering engine, and rudder is put plate and is placed in control cabinet, is connect by connector with bottom plate,
The electric steering engine is connected by steering engine interface with bottom plate；Further include the transmission output mechanism being connected with electric steering engine, is used for root
The deflection that respective angles are generated according to the steering engine axis of the instruction control electric steering engine of control cabinet, controls the flight attitude of target missile.
Preferably, above-mentioned more running fire target missile control systems, electric steering engine include duck rudder steering engine and three common steering engines；Duck
Rudder steering engine is placed in steering gear flat, is connected with transmission output mechanism, common steering engine is placed in enging cabin；Duck rudder steering engine includes
Group amplifier and angular transducer, flight-control computer export rudder machine control signal, after group amplifier conditioning amplification
Motor control signal is generated, control motor rotation is so that steering engine axis deflects；The deflection angle of steering engine axis is through angle sensor simultaneously
Device is transformed to voltage signal, feeds back to group amplifier, constitutes the closed-loop control of rudder system.
Preferably, above-mentioned more running fire target missile control systems, Gyro include three rate gyroscopes, gimbal, electricity
Source plate conciliates tuned plate, and rate gyroscope is mounted on gimbal, and power panel reconciliation tuned plate is connected by connector with bottom plate, gyro
Bracket is electrically connected by connecting cable and bottom plate；Three rate gyroscopes are for measuring sensitive guided missile under missile coordinate system
Three axis angular rate components；The working power of Gyro is provided by power panel, solves demodulator circuit and rate gyroscope on tuned plate
An angular velocity measurement system is formed together, completes the Operating In Persistent Current Mode of rate gyroscope and the sampling processing of signal；
Flight control computer includes connected computer plate and GPS plate；Computer plate is connected by connector with bottom plate, GPS
Plate is mounted on computer plate, realizes the electrical connection with computer by connector；Flight control computer is for acquiring gyro group
It closes, the information of GPS and altimeter, carries out posture, position resolving, carry out flying to control resolving according to control law, output steering engine controls
Signal controls rudder system work, guarantees that target missile flies by scheduled track；And the state parameter in target missile flight course is sent
To telemetering radio station.
Preferably, above-mentioned more running fire target missile control systems are additionally provided with emulation interface on bottom plate, and emulation interface is for controlling
System carries out carrying out data acquisition and communication when Hardware-in-loop Simulation Experimentation；Telemetering electric plates are equipped with de- interface, control cabinet connects
Connection interface, and test and protection interface for distinguishing control system working condition are additionally provided with for connecing in enging cabin
Receive the separation interface of target missile separation signal and the igniting interface of ignition signal.
Preferably, above-mentioned more running fire target missile control systems substitute transmitting station, the portable master control with portable master station
Platform is integral type industrial personal computer, including controller, On-off signal board, output switch parameter board, serial ports board and the more function of AD/DA
It can data board；Portable master station switches target missile transmission channel, N number of signal in transmitter control station for exporting control signal
Conditioning plate is respectively sent to test interface and emission interface after carrying out conditioning parsing to received control signal, controls corresponding target missile
Execute transmitting movement.
Preferably, above-mentioned more running fire target missile control systems, further include the combined test stand being connected with portable master station, described
Combined test stand includes signal regulating panel, adapter panel and AC/DC power supply, and signal regulating panel is mainly used for realizing that ground supplies
Electricity, simulation power supply, unlock, boosting, activation, power switching control, AD is acquired and ground bounce communication function, has on adapter panel
Indicator light and button；Signal regulating panel exports the test instruction that portable master station issues and testing process to the electrical of target missile
Cabin or control cabinet, the test or integrated testability of the corresponding bay section of control target missile.
Preferably, above-mentioned more running fire target missile control systems, further include telemetering console, and the telemetering console is for receiving
Target missile flight course passes through the target missile state parameter that wireless device passes down, and sends it to transmitting station or portable master control
Platform realizes real-time monitoring and control to target missile state of flight.
Preferably, above-mentioned more running fire target missile control systems, portable master station further include switch, button, indicator light, with
And keyboard, display and mouse convenient for human-computer interaction, the keyboard, display and mouse pass through subrack card and portable master
Platform is controlled to be connected.
In general, through the invention it is contemplated above technical scheme is compared with the prior art, can obtain down and show
Beneficial effect:
(1) a kind of more running fire target missile control systems provided by the invention are made by carrying out program setting to transmitting station
Transmitting station has more running fire target missile emission functions；The signal regulating panel to match with target missile number is set in transmitter control station
And emission interface, emission interface is sent after carrying out conditioning parsing to received control instruction, it is dynamic that control target missile executes continuous transmitting
Make, improve target missile for target ability.
(2) a kind of more running fire target missile control systems provided by the invention are replaced using the portable console of customization all-in-one machine
Emit station, portable console other than having the target missile emission control function of transmitting station, may be used also by portable master station
It is small in size easy to carry for testing each bay section of target missile, facilitate its transformation to use position；
(3) a kind of more running fire target missile control systems provided by the invention, the GPS installed in target missile flight subsystem can
Target missile is improved for the lateral range and security reliability in target；Rudder system select harmonic wave electric rudder system, have it is small in size,
The characteristics of dynamic characteristic is good, strong robustness, the control suitable for small projectile；Duck rudder steering engine includes that group amplifier and angle pass
Sensor, flight-control computer export rudder machine control signal, generate motor control signal after group amplifier conditioning, amplification,
Motor rotation is controlled so that steering engine axis deflects；The deflection angle of steering engine axis is transformed to voltage signal through angular transducer simultaneously,
Group amplifier is fed back to, the closed-loop control of rudder system is constituted, improves the sensitivity of target missile flight control.
Detailed description of the invention
Fig. 1 is the tomograph of target missile flight subsystem in more running fire target missile control systems provided by the invention；
Fig. 2 is the module frame chart of target missile flight subsystem；
Fig. 3 is the composition schematic diagram of ground control subsystem in more running fire target missile control systems provided by the invention；
Fig. 4 is the module organigram of ground control subsystem；
Fig. 5 is the appearance diagram of convenient master station in ground control subsystem provided by the invention；
Fig. 6 is the realization figure for emitting the target missile emission control function of station；
Fig. 7 is the realization figure of the target missile test and target missile emission control function of portable master station.
Specific embodiment
In order to make the objectives, technical solutions, and advantages of the present invention clearer, with reference to the accompanying drawings and embodiments, right
The present invention is further elaborated.It should be appreciated that the specific embodiments described herein are merely illustrative of the present invention, and
It is not used in the restriction present invention.As long as in addition, technical characteristic involved in the various embodiments of the present invention described below
Not constituting a conflict with each other can be combined with each other.
A kind of more running fire target missile control systems provided by the present invention, including target missile flight subsystem and ground control
Subsystem；
Target missile flight subsystem is the core of target missile, including target missile control cabinet, electrical cabin and steering gear flat, target missile flight
Control subsystem is mainly used for attitude angular rate signal, altitude signal and the GPS in three directions when real-time measurement target missile flight
Signal forms rudder machine control signal according to control law, controls target missile attitude stabilization, is climbed by the program of setting, fixed height
It is flat to fly and course position control.
Ground control subsystem includes portable master station, transmitting station, transmitter control station, telemetering console and synthesis
Testboard can satisfy target missile test, portable transmitting, vehicle transmitting, multiple target missile (1 to 4 hair) continuous emission function needs；
Wherein, portable master station is for control signal source needed for providing ground control subsystem, to target missile state
It is tested, cooperation transmitter control station completes the emission control to target missile, has the continuous emission control function of four hair target missiles；
Transmitting station is completed for control signal source needed for providing ground control subsystem, cooperation transmitter control station
Transmitting docking test and emission control to target missile, have the continuous emission control function of four hair target missiles；
Transmitter control station is used to receive portable master station or emit the control signal of station, completes the transmitting to target missile
Control；
Combined test stand is to provide the test platform of test in the control subsystem of ground for each bay section of target missile, according to portable
The test of electrical cabin, control cabinet test and entire control system to target missile are completed in the test instruction and testing process that master station issues
Test；
Telemetering console is ground bounce Communication receiving station, passes through the target missile that wireless device passes down for receiving target missile flight course
State parameter realizes the real time monitoring to target missile state.
More running fire target missile control systems provided in an embodiment of the present invention are described in detail with reference to the accompanying drawing.
One, target missile flight subsystem
Fig. 1 is the tomograph of target missile flight subsystem, and Fig. 2 is the module frame of target missile flight subsystem
Figure；As shown in Fig. 2, target missile flight subsystem includes that control cabinet, electrical cabin and rudder system, rudder system are divided into steering gear flat and hair
Two, motivation cabin part, control cabinet are connected with electrical cabin, steering gear flat and enging cabin respectively, electrical cabin respectively with control cabinet and hair
Motivation cabin is connected；Control cabinet and steering gear flat constitute the control unit of target missile flight subsystem, are used for real-time measurement target missile
Attitude angular rate signal, altitude signal and the GPS signal in three directions when flight form steering engine control letter according to control law
Number, control target missile posture changing；Electrical cabin is defeated for turn electric power supply control of target missile flight subsystem and priming system instruction
Out.
Control cabinet includes Gyro, flight control computer, altimeter and bottom plate；Gyro, flight control computer and height
Table is connected with bottom plate, and bottom plate is equipped with electrical cabin connecting interface and emulation interface；Control cabinet by electrical cabin connecting interface with
Communication connection is established in electrical cabin, and emulation interface is used to carry out data acquisition when control system carries out Hardware-in-loop Simulation Experimentation and lead to
Letter；
Gyro includes gimbal, power panel reconciliation tuned plate, and power panel conciliates tuned plate and passes through connector and bottom plate phase
Even, gimbal is electrically connected by connecting cable and bottom plate；Gyro include three rate gyroscopes, Gyro with
Target missile body is fixedly connected, and is the sensing unit of target missile flight subsystem, for measuring sensitive guided missile in missile coordinate system
Under three axis angular rate components.The working power of Gyro is provided by power panel, and the demodulator circuit solved on tuned plate is gyro group
It closes most important electronic circuit and rate gyroscope and forms an angular velocity measurement system together, complete the closure work of rate gyroscope
The sampling processing of work and signal.
Flight control computer includes connected computer plate and GPS plate；Computer plate is connected by connector with bottom plate, GPS
Plate is mounted on computer plate, realizes the electrical connection with computer by connector；The function of flight control computer is acquisition top
Spiral shell combination, GPS and altimeter information, carry out posture, position resolve, according to control law carry out fly control resolve, export steering engine
Signal control rudder system work is controlled, guarantees that target missile flies by scheduled track；Target missile can be improved in for target in the GPS of installation
Lateral range and security reliability, flight control computer pass through RS232 telemetry interface for the state parameter in target missile flight course
It is sent to electrical cabin.The processing chip of flight control computer uses the TMS32C6000 series DSP of TI (Texas Instrument) company, should
Dsp chip can execute monocyclic fixed point and floating point instruction under the running frequency of 225MHz, meet and resolve requirement.
Rudder system selects harmonic wave electric rudder system, has the characteristics that small in size, dynamic characteristic is good, strong robustness, is suitable for
The control of small projectile.Rudder system includes that rudder puts plate and four electric steering engines, and rudder is put plate and is placed in control cabinet, and connector is passed through
It links together with bottom plate, four electric steering engines include duck rudder steering engine and steering engine I, steering engine II, steering engine III, and duck rudder steering engine is placed on
In steering gear flat, it is connected by duck rudder interface with the bottom plate in control cabinet, steering engine I, steering engine II and steering engine III are individually positioned in target missile
Port wing, on starboard wing and tail, steering engine I, steering engine II, steering engine III pass through steering engine interface I, the steering engine in enging cabin respectively
Interface II, steering engine interface III are connected with bottom plate；It is additionally provided with separation interface and igniting interface in enging cabin, is respectively used to receive electricity
The target missile separation command and firing command that gas cabin issues；Steering gear flat further includes a set of transmission output mechanism, and function is according to control
The instruction requirement in cabin processed makes the steering engine axis of duck rudder steering engine generate the deflection of respective angles.Duck rudder steering engine include group amplifier and
Angular transducer, flight-control computer export rudder machine control signal, generate motor control after group amplifier conditioning, amplification
Signal, control motor rotation is so that steering engine axis deflects；The deflection angle of steering engine axis is transformed to voltage through angular transducer simultaneously
Signal feeds back to group amplifier, constitutes the closed-loop control of rudder system.
Electrical cabin includes telemetering electric plates, battery, radar cell and telemetering radio station, and the working power of telemetering electric plates is by electricity
Pond provides, and battery, radar cell and telemetering radio station are connected with telemetering electric plates, and telemetering electric plates are equipped with de- interface, use
In the test and protection interface and control cabinet connecting interface of distinguishing control system working condition, telemetering radio station by telemetry interface with
Control cabinet establishes communication connection, to receive the target missile state parameter of flight control computer sending；Telemetering electric plates also with separation interface
It is connected with igniting interface, control target missile executes separation and firing action.The function in electrical cabin is according to flight control computer and ground
The control instruction of control subsystem completes the power supply of target missile system, turns the output of electricity and ignition signal, and control target missile executes separation
And firing action, it receives the telemetry that flight control computer issues and is transmitted to ground control subsystem.
Two, ground control subsystem
Fig. 3 is the composition schematic diagram of ground control subsystem, and Fig. 4 is the module organigram of ground control subsystem；
As shown in Figure 3 and Figure 4, ground control subsystem includes transmitting station, transmitter control station, portable master station, integration test
Platform and surface telemetry system；
Wherein, transmitting station is mounted in the cabinet of command and control vehicle, including display, station and industrial personal computer, is shown
Show device and industrial personal computer is standard subrack, selects damping escope to improve the use longevity of transmitting station in the presence of a harsh environment
Life, station include switch, indicator light, keyboard and mouse, and transmitting station provides working power by 220V alternating current；Emission control
Platform is mounted on car launcher, including adapter and AC/DC power case, is equipped in adapter for connecting with transmitting station
Mating interface controls cable by 80m between transmitter control station and transmitting station and is connected；The present embodiment is with the running fire of four hair target missiles
It is illustrated for control, to realize four hair target missile running fires, adapter further includes four test interfaces, four emission interfaces and four
A signal regulating panel, AC/DC power case include two groups of AC/DC power supplys and power interface；Each test interface passes through survey respectively
Examination cable is connected with a hair target missile, completes target missile transmitting docking test；Each emission interface passes through control cable and a hair respectively
Target missile is connected, and realizes the emission control of four hair target missiles；Four signal regulating panels and four hair target missiles correspond, for received
Control instruction is sent to test interface or emission interface after carrying out conditioning parsing, and control target missile executes corresponding actions；220V alternating current
Transmitter control station is accessed by power interface, two-way 27V power supply is converted to by AC/DC power supply, is all the way rudder system power supply, separately
It powers all the way for control system；Every group of AC/DC power supply is exported including four tunnels, the urban electric power switch 220V and AC/DC switch of power supply output
In the interior long-range control of command and control.
Emit station and be used as remote control center, real time monitoring target missile state simultaneously exports control instruction and is emitted into target missile
Row remote control；Transmitter control station emits signal converting control platform as target missile, is responsible for completing battery activated signal, turns telecommunications
Number, the conversions of the signal of interest such as unlocking signal, boosting ignition signal, be completed at the same time target missile signal back production.Fig. 6 is transmitting station
With the module frame chart of transmitter control station, the industrial personal computer for emitting station includes controller, On-off signal board, output switch parameter
Board, serial ports board and AD/DA multi-functional data board are acquired and are converted for data；In addition, switch on station, referring to
Show that lamp, button and human-computer interaction interface turn wire box by inside and be transferred on the external socket of cabinet, operator is in human-computer interaction
Target missile state in place is identified on interface in real time, and successively carries out transmitting docking test to N number of target missile by band switch, is tested
Transmission channel is switched fast by band switch at rear, realizes the continuous emission control of four hair target missiles.Transmitting station passes through hair
Penetrate control cable 1, emission control cable 2, emission control cable 3, emission control cable 4 respectively with the signal in transmitter control station
Conditioning plate 1, signal regulating panel 2, signal regulating panel 3, signal regulating panel 4 are connected, to control target missile 1, target missile 2, target missile 3, target missile 4
Transmitting；Telemetering console is connected with transmitting station, and telemetering console is ground bounce Communication receiving station, for receiving target missile flight
Received target missile state parameter is sent to transmitting behaviour by the state parameter that process is passed down by wireless device, telemetering console
Make platform, to carry out implementing monitoring and adjustment to target missile state.
Since transmitting station is only used for providing man-machine interactive platform on command and control vehicle, have a single function, volume it is big and
It is not portable, therefore a kind of portable master station is present embodiments provided to substitute transmitting station, appearance diagram such as Fig. 5 institute
Show；Portable master station is the dedicated KVM integral type industrial personal computer of customization, including display, keyboard and mouse, switch, button and instruction
Lamp is mainly responsible for man-machine interaction, conveys test instruction and testing process, the combined test stand conduct being connected with portable master station
Signal adaptation transfer platform, control cabinet or electrical cabin by output after portable master station control instruction to target missile, completes target missile
Corresponding bay section test or integration test.Portable master station is consistent with the function of transmitting station and interface, but in addition to having hair
It penetrates outside the target missile emission control function of station, portable master station can also be used to test each bay section of target missile.
Fig. 7 is the realization figure of the target missile test and target missile emission control function of portable master station, as shown in fig. 6, target missile
Test function realizes that the industrial personal computer of portable master station includes controller, switching value by portable master station and combined test stand
Input card, output switch parameter board, serial ports board and AD/DA multi-functional data board；Portable master station further include switch,
Button, indicator light, and convenient for the keyboard, display and mouse of human-computer interaction, keyboard, display and mouse pass through subrack card
It is connected with portable master station.
Combined test stand includes signal regulating panel, adapter panel and AC/DC power supply, and signal regulating panel is mainly used for realizing
Surface power supply, simulation power supply, unlock, boosting, activation, power switching control, AD acquisition and ground bounce communication function, adapter panel
It is upper that there is indicator light and button；Signal regulating panel by the control instruction that portable master station issues export to target missile electrical cabin or
Control cabinet, the test or integrated testability of the corresponding bay section of control target missile.
Target missile emission control function is realized that portable master station passes through transmitting control by portable master station and transmitter control station
Cable 1 processed, emission control cable 2, emission control cable 3, emission control cable 4 respectively with the signal condition in transmitter control station
Plate 1, signal regulating panel 2, signal regulating panel 3, signal regulating panel 4 are connected, to control target missile 1, target missile 2, target missile 3, target missile 4 respectively
Transmitting, transmitter control station further includes for providing the AC/DC power supply of working power for signal regulating panel, and telemetering console will connect
The target missile state parameter of receipts is sent to portable master station, and portable master station carries out implementing monitoring and adjustment to target missile state.
Transmitting station and portable master station are provided with target missile emission control function, and the two is used equally for 1 to 4 hair target missile
Emission control, transmitting station, which is only used for accusing, provides man-machine interactive platform on vehicle, has a single function, structural strength is high, cost
It is lower；And portable master station takes into account target missile test and target missile emission control, and easy to carry, its transformation is facilitated to use position.
More running fire target missile control systems provided by the invention grasp transmitting by carrying out program setting to transmitting station
Have more running fire target missile emission functions as platform；The signal regulating panel to match with target missile number and transmitting are set in transmitter control station
Interface sends emission interface after carrying out conditioning parsing to received control instruction, and control target missile executes continuous transmitting movement, improves
Target missile for target ability；Transmitting station is replaced using the portable console of customization all-in-one machine, portable console is in addition to having hair
It penetrates outside the target missile emission control function of station, portable master station can also be used to test each bay section of target missile, small in size
It is easy to carry, facilitate its transformation to use position.
As it will be easily appreciated by one skilled in the art that the foregoing is merely illustrative of the preferred embodiments of the present invention, not to
The limitation present invention, any modifications, equivalent substitutions and improvements made within the spirit and principles of the present invention should all include
Within protection scope of the present invention.
Claims (9)
1. a kind of more running fire target missile control systems, which is characterized in that control subsystem including target missile flight subsystem and ground
System；
The target missile flight subsystem be mainly used for the attitude angular rate signal in three directions when real-time measurement target missile flight,
Altitude signal and GPS signal form rudder machine control signal according to control law, target missile attitude stabilization are controlled, by the journey of setting
Sequence is climbed, Ding Gaoping flies and course position control；
The ground control subsystem includes that the connected transmitting station and transmitter control station of emission control cable, institute are covered by N
Transmitting station is stated for control signal needed for providing ground control subsystem, switches the transmission channel of different target missiles, is cooperated
The transmitter control station completes transmitting docking test and emission control to target missile, realizes that N sends out the continuous emission control function of target missile,
Wherein, N is natural number；
The transmitter control station is used to receive the control signal of transmitting station, completes the emission control to target missile；Emission control
Platform includes N number of signal regulating panel, N number of test interface and N number of emission interface, and n-th target missile is tested by test cable and n-th
Interface is connected, and is connect by firing cable with n-th emission interface；The control that the signal regulating panel issues transmitting station
Signal is sent to the test interface and emission interface after carrying out conditioning parsing, controls corresponding target missile and executes transmitting movement；
The target missile flight subsystem includes control cabinet, electrical cabin and rudder system, the electrical cabin and rudder system with control
Cabin processed is connected, and the control cabinet and rudder system constitute the control unit of target missile flight subsystem, and the electrical cabin is used for
Target missile flight subsystem turns electric power supply control and priming system instruction output；
The control cabinet includes Gyro, flight control computer, altimeter and bottom plate；The Gyro, flight control computer and
Altimeter is connected with bottom plate, and the bottom plate is equipped with electrical cabin connecting interface；
The electrical cabin includes telemetering electric plates, battery and telemetering radio station, and the working power of the telemetering electric plates is mentioned by battery
For the battery and telemetering radio station are connected with telemetering electric plates, and the telemetering radio station passes through in telemetry interface and control cabinet
Bottom plate is connected, to receive the target missile state parameter of flight control computer sending；
The rudder system includes that rudder puts plate and electric steering engine, and the rudder is put plate and is placed in control cabinet, and connector and bottom plate are passed through
Connection, the electric steering engine are connected by steering engine interface with bottom plate；Further include the transmission output mechanism being connected with electric steering engine, uses
The deflection of respective angles is generated in the steering engine axis that the instruction according to control cabinet controls electric steering engine, controls the flight attitude of target missile；
The electric steering engine includes duck rudder steering engine and three common steering engines；The duck rudder steering engine includes that group amplifier and angle pass
The rudder machine control signal of sensor, flight-control computer output generates motor control letter after group amplifier conditioning amplification
Number, motor rotation is controlled so that steering engine axis deflects according to the motor control signal；The deflection angle of steering engine axis is through the angle
Degree sensor is converted to voltage signal and feeds back to group amplifier, constitutes the closed-loop control of rudder system.
2. a kind of more running fire target missile control systems as described in claim 1, which is characterized in that the transmitting station includes work
Control machine, display and station, the industrial personal computer include controller, On-off signal board, output switch parameter board, subrack
Card and AD/DA multi-functional data board, the station include switch, indicator light, keyboard and mouse, the display, keyboard
Human-computer interaction interface is constituted with mouse, operator obtains the state in place of target missile by the human-computer interaction interface, and passes through
The transmission channel of the switching difference target missile.
3. a kind of more running fire target missile control systems as described in claim 1, which is characterized in that the duck rudder steering engine is placed on rudder
In cabin, it is connected with the transmission output mechanism, the common steering engine is placed in enging cabin.
4. a kind of more running fire target missile control systems as claimed in claim 3, which is characterized in that the Gyro includes three
Rate gyroscope, gimbal, power panel conciliate tuned plate, and the rate gyroscope is mounted on gimbal, the power panel reconciliation
Tuned plate is connected by connector with bottom plate, and the gimbal is electrically connected by connecting cable and bottom plate；The rate
Gyro is for measuring three axis angular rate components of the sensitive guided missile under missile coordinate system；The working power of Gyro is by the electricity
Source plate provides, and the demodulator circuit and rate gyroscope on the solution tuned plate form an angular velocity measurement system together, completes rate
The Operating In Persistent Current Mode of gyro and the sampling processing of signal；
The flight control computer includes connected computer plate and GPS plate；The computer plate is connected by connector with bottom plate,
The GPS plate is mounted on computer plate, realizes the electrical connection with computer plate by connector；Flight control computer is for adopting
Collect the information of Gyro, GPS and altimeter, carry out posture, position resolving, carries out flying to control resolving according to control law, output
Rudder machine control signal controls rudder system work, guarantees that target missile flies by scheduled track；And by the state in target missile flight course
Parameter is sent to telemetering radio station.
5. a kind of more running fire target missile control systems as described in claim 1, which is characterized in that the bottom plate further includes that emulation connects
Mouthful, the emulation interface is used to carry out data acquisition and communication when control system carries out Hardware-in-loop Simulation Experimentation；The telemetering
Electric plates are equipped with de- interface, control cabinet connecting interface, and test and protection for distinguishing control system working condition
Interface is additionally provided with the igniting interface of the separation interface and ignition signal for receiving target missile separation signal in enging cabin.
6. a kind of more running fire target missile control systems as claimed in any one of claims 1 to 5, which is characterized in that with portable master control
Platform substitution transmitting station, the portable master station are integral type industrial personal computer, including controller, On-off signal board, switch
Measure output board card, serial ports board and AD/DA multi-functional data board；Portable master station is used to export the control signal of target missile transmitting
And switching target missile transmission channel, the signal regulating panel in transmitter control station is sent out respectively after carrying out conditioning parsing to the control signal
It send to test interface and emission interface, controls corresponding target missile and execute transmitting movement.
7. a kind of more running fire target missile control systems as claimed in claim 6, which is characterized in that further include and portable master station phase
Combined test stand even, the combined test stand includes signal regulating panel, adapter panel and AC/DC power supply, the signal tune
It manages plate and communicates function for realizing surface power supply, simulation power supply, unlock, boosting, activation, power switching control, AD acquisition and ground bounce
Can, there is indicator light and button on the adapter panel；The test that signal regulating panel issues portable master station is instructed and is surveyed
Examination process is exported to the electrical cabin of target missile or control cabinet, controls the test or integrated testability of the corresponding bay section of target missile.
8. a kind of more running fire target missile control systems as claimed in claim 6, which is characterized in that further include telemetering console, institute
It states telemetering console and passes through the target missile state parameter that wireless device passes down for receiving target missile flight course, and send it to hair
Station or portable master station are penetrated, realizes real-time monitoring and control to target missile state of flight.
9. a kind of more running fire target missile control systems as claimed in claim 6, which is characterized in that the portable master station further includes
Switch, button, indicator light, and convenient for the keyboard, display and mouse of human-computer interaction, the keyboard, display and MouseAcross
Serial ports board is crossed to be connected with portable master station.
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| KR101199449B1 (en) * | 2009-09-02 | 2012-11-09 | 국방과학연구소 | Controlling apparatus in the batte system of naval vessel filtering targets real time, and the method using the same, and computer readable medium recording program for performing the same |
| US8634974B2 (en) * | 2012-01-09 | 2014-01-21 | Google Inc. | Using predicted movement to maintain optical-communication lock with nearby balloon |
| CN103471468B (en) * | 2013-08-22 | 2015-05-06 | 北京航空航天大学 | Universal telecontrol and telemetry system for aviation tow target |
| CN204514195U (en) * | 2014-12-28 | 2015-07-29 | 西安北方惠安化学工业有限公司 | A kind of high-performance cruise formula target missile |
| CN204442571U (en) * | 2015-03-25 | 2015-07-01 | 中国航空工业集团公司上海航空测控技术研究所 | A kind of supersonic speed target missile missile-borne monitoring system |
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