CN108319189A - 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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- CN108319189A CN108319189A CN201810011630.7A CN201810011630A CN108319189A CN 108319189 A CN108319189 A CN 108319189A CN 201810011630 A CN201810011630 A CN 201810011630A CN 108319189 A CN108319189 A CN 108319189A
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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；Attitude angular rate signal, altitude signal and the GPS signal in three directions when the target missile flight subsystem is mainly used for measuring target missile flight in real time, servos 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 covering the connected transmitting operation console and transmitter control station of emission control cable by N, the transmitting operation console is used to provide the control signal needed for the control subsystem of ground, coordinate transmitter control station to complete transmitting docking test and emission control to target missile, has the N hair continuous emission control functions of target missile；The present invention can realize the emission control and test of more running fire target missiles, improve target missile for target ability, and it is small 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 technology
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
The increasingly complex of war environment, usually puts forward higher requirements target missile for target ability,
Target missile is to provide target in the experiment 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
Collecting the system of target becomes active demand.
Invention content
For the disadvantages described above or Improvement requirement of the prior art, the present invention provides a kind of more running fire target missile control systems,
The system makes transmitting operation console have more running fire target missile emission functions by carrying out program setting to transmitting operation console；Emitting
The signal regulating panel and emission interface that setting matches with target missile number in console, conditioning parsing is carried out to the control instruction of reception
After send emission interface, control target missile executes continuous transmitting action, 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 in real time measure target missile flight when three directions attitude angular rate signal,
Altitude signal and GPS signal form servos control signal according to control law, control target missile attitude stabilization, by the journey of setting
Sequence is climbed, Ding Gaoping flies and course position control；
Ground control subsystem includes covering the connected transmitting operation console and transmitter control station of emission control cable, hair by N
Operation console is penetrated for providing the control signal needed for the control subsystem of ground, 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 operation console, 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 the control instruction of reception
After be sent to test interface and emission interface, control corresponding target missile and execute transmitting action.
Preferably, above-mentioned more running fire target missile control systems, transmitting operation console includes industrial personal computer, display and operation console,
Industrial personal computer includes controller, On-off signal board, output switch parameter board, serial ports board and AD/DA multi-functional data boards,
Operation console includes switch, indicator light, keyboard and mouse, and display, keyboard and mouse constitute human-computer interaction interface, and operating personnel are logical
It crosses human-computer interaction interface and obtains the state in place of target missile, and pass 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 is sent out；
Rudder system includes that rudder puts plate and electric steering engine, and rudder is put plate and is placed in control cabinet, is connect with bottom plate by connector,
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 servos 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
Holder 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 plates；Computer plate is connected by connector with bottom plate, GPS
Plate is mounted on computer plate, and the electrical connection with computer is realized 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, export servos control
Signal controls rudder system work, ensures 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 the test for distinguishing control system working condition and protection interface are additionally provided with for connecing in enging cabin
Receive the igniting interface of the separation interface and ignition signal of target missile separation signal.
Preferably, above-mentioned more running fire target missile control systems substitute transmitting operation console, 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 work(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 the control signal of reception, controls corresponding target missile
Execute transmitting action.
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 supplys, 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 is sent out 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
The target missile state parameter that target missile flight course is passed down by wireless device, and send it to transmitting operation console or portable master control
Platform realizes the 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 operation console
Transmitting operation console has more running fire target missile emission functions；The signal regulating panel that setting matches with target missile number in transmitter control station
And emission interface, emission interface is sent after carrying out conditioning parsing to the control instruction of reception, 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 operation console, portable console other than having the target missile emission control function of transmitting operation console, may be used also by portable master station
It is small 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,
The characteristics of dynamic characteristic is good, strong robustness is suitable for the control of small projectile；Duck rudder steering engine includes that group amplifier and angle pass
Sensor, flight-control computer export servos control signal, and motor control signal is generated 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.
Description of the drawings
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 structure schematic diagram 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 the target missile emission control function of emitting operation console；
Fig. 7 is the realization figure of the target missile test and target missile emission control function of portable master station.
Specific implementation mode
In order to make the purpose , technical scheme and advantage of the present invention be 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
It does not constitute a conflict with each other and 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
Attitude angular rate signal, altitude signal and the GPS in three directions when control subsystem is mainly used for measuring target missile flight in real time
Signal forms servos 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 operation console, transmitter control station, telemetering console and synthesis
Testboard disclosure satisfy that target missile test, portable transmitting, vehicle transmitting, multiple target missile (1 to 4 hair) continuous emission function needs；
Wherein, portable master station is used to provide the control signal source needed for the control subsystem of ground, 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 operation console is used to provide the control signal source needed for the control subsystem of ground, and cooperation transmitter control station is completed
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 operation console, completes the transmitting to target missile
Control；
Combined test stand is the test platform for providing 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 is sent out
Test；
Telemetering console is ground bounce Communication receiving station, the target missile passed down by wireless device 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 below in conjunction with the accompanying drawings.
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, which includes control cabinet, electrical cabin and rudder system, rudder system, is 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, for measuring target missile in real time
Attitude angular rate signal, altitude signal and the GPS signal in three directions when flight form servos 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
Go 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
Electrical cabin, which is established, communicates connection, 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 reconciliation tuned plate 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 plates；Computer plate is connected by connector with bottom plate, GPS
Plate is mounted on computer plate, and the electrical connection with computer is realized 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, ensures 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 is by RS232 telemetry interfaces by 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 DSPs 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, 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 with the bottom plate in control cabinet by duck rudder interface, 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 is sent out；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 servos control signal, and motor control is generated 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 that flight control computer is sent out；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 is sent out 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 structure schematic diagram of ground control subsystem；
As shown in Figure 3 and Figure 4, ground control subsystem includes transmitting operation console, transmitter control station, portable master station, integration test
Platform and surface telemetry system；
Wherein, transmitting operation console is mounted in the cabinet of command and control vehicle, including display, operation console and industrial personal computer, is shown
Show that device and industrial personal computer are standard subrack, selects damping escope to improve the use longevity of transmitting operation console in the presence of a harsh environment
Life, operation console include switch, indicator light, keyboard and mouse, and transmitting operation console provides working power by 220V alternating currents；Emission control
Platform is mounted on car launcher, including adapter and AC/DC power cases, is equipped in adapter for connecting with transmitting operation console
Mating interface controls cable by 80m between transmitter control station and transmitting operation console 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 cases 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 is respectively by controlling cable and a hair
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 reception
Control instruction is sent to test interface or emission interface after carrying out conditioning parsing, and control target missile executes corresponding actions；220V alternating currents
Transmitter control station is accessed by power interface, two-way 27V power supplys are converted to by AC/DC power supplys, is powered all the way for rudder system, separately
System power supply in order to control all the way；Every group of AC/DC power supply is exported including four tunnels, the urban electric power switch 220V and AC/DC switchs of power supply output
In command and control car remote control.
Emitting operation console is used as remote control center, real time monitoring target missile state simultaneously to export control instruction and be 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 operation console
With the module frame chart of transmitter control station, the industrial personal computer for emitting operation console includes controller, On-off signal board, output switch parameter
Board, serial ports board and AD/DA multi-functional data boards are acquired and are converted for data；In addition, switch on operation console, 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, operating personnel are in human-computer interaction
Target missile state in place is identified on interface in real time, and carries out transmitting docking test successively 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 operation console 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 operation console, and telemetering console is ground bounce Communication receiving station, for receiving target missile flight
The target missile state parameter of reception 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 operation console 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 operation console, appearance diagram such as Fig. 5 institutes
Show；Portable master station is the special KVM integral types 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 operation console and interface, but in addition to having hair
It penetrates outside the target missile emission control function of operation console, 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 boards；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 supplys, and signal regulating panel is mainly used for realizing
Surface power supply, simulation power supply, unlock, boosting, activation, power switching control, AD acquisitions 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 is sent out 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 is controlled by emitting 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 the AC/DC power supplys for providing 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 operation console 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 operation console is only used for accusing provides man-machine interactive platform on vehicle, has a single function, structural strength is high, cost
It is relatively low；And portable master station takes into account target missile test and target missile emission control, and it is easy to carry, facilitate its transformation to use position.
More running fire target missile control systems provided by the invention make transmitting grasp by carrying out program setting to transmitting operation console
Have more running fire target missile emission functions as platform；The signal regulating panel and transmitting that setting matches with target missile number in transmitter control station
Interface sends emission interface after carrying out conditioning parsing to the control instruction of reception, and control target missile executes continuous transmitting action, improves
Target missile for target ability；Transmitting operation console 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 operation console, portable master station can also be used to test each bay section of target missile, small
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, all within the spirits and principles of the present invention made by all any modification, equivalent and improvement etc., should all include
Within protection scope of the present invention.
Claims (10)
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 in real time measure target missile flight when three directions attitude angular rate signal,
Altitude signal and GPS signal form servos control signal according to control law, control target missile attitude stabilization, by the journey of setting
Sequence is climbed, Ding Gaoping flies and course position control；
The ground control subsystem includes covering the connected transmitting operation console and transmitter control station of emission control cable, institute by N
It states transmitting operation console to be used to provide the control signal needed for the control subsystem of ground, switches the transmission channel of different target missiles, coordinate
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 operation console, 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 with n-th emission interface by firing cable；The control that the signal regulating panel sends out transmitting operation console
Signal is sent to the test interface and emission interface after carrying out conditioning parsing, controls corresponding target missile and executes transmitting action.
2. a kind of more running fire target missile control systems as described in claim 1, which is characterized in that the transmitting operation console includes work
Control machine, display and operation console, the industrial personal computer include controller, On-off signal board, output switch parameter board, subrack
Card and AD/DA multi-functional data boards, the operation console include switch, indicator light, keyboard and mouse, the display, keyboard
Human-computer interaction interface is constituted with mouse, operating personnel obtain the state in place of target missile by the human-computer interaction interface, and pass through
The transmission channel of the switching difference target missile.
3. a kind of more running fire target missile control systems as claimed in claim 1 or 2, which is characterized in that the target missile flight control
Subsystem includes control cabinet, electrical cabin and rudder system, and the electrical cabin and rudder system are connected with control cabinet, the control cabinet and
Rudder system constitutes the control unit of target missile flight subsystem, and the electrical cabin turns for target missile flight subsystem
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 carried 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 that flight control computer is sent out；
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 for controlling electric steering engine according to the instruction of control cabinet, controls the flight attitude of target missile.
4. a kind of more running fire target missile control systems as claimed in claim 3, which is characterized in that the electric steering engine includes duck rudder
Steering engine and three common steering engines；The duck rudder steering engine is placed in steering gear flat, is connected with the transmission output mechanism, described common
Steering engine is placed in enging cabin；The duck rudder steering engine includes group amplifier and angular transducer, and flight-control computer is defeated
The servos control signal gone out generates motor control signal after group amplifier conditioning amplification, is controlled and is believed according to the motor
The rotation of number control motor is so that steering engine axis deflects；The deflection angle of steering engine axis is converted to voltage signal through the angular transducer
And group amplifier is fed back to, constitute the closed-loop control of rudder system.
5. a kind of more running fire target missile control systems as described in claim 3 or 4, which is characterized in that the Gyro includes
Three rate gyroscopes, 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；It is described
Rate gyroscope is for measuring three axis angular rate components of the sensitive guided missile under missile coordinate system；The working power of Gyro is by institute
Power panel offer is stated, the demodulator circuit and rate gyroscope on the solution tuned plate form an angular velocity measurement system together, complete
The Operating In Persistent Current Mode of rate gyroscope and the sampling processing of signal；
The flight control computer includes connected computer plate and GPS plates；The computer plate is connected by connector with bottom plate,
The GPS plates are mounted on computer plate, and the electrical connection with computer plate is realized 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
Servos control signal controls rudder system work, ensures that target missile flies by scheduled track；And by the state in target missile flight course
Parameter is sent to telemetering radio station.
6. a kind of more running fire target missile control systems as claimed in claim 3, 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 for detaching the separation interface and ignition signal of signal for receiving target missile in enging cabin.
7. such as a kind of more running fire target missile control systems of claim 1~6 any one of them, which is characterized in that with portable master control
Platform substitutes transmitting operation console, and the portable master station is 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 boards；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 action.
8. a kind of more running fire target missile control systems as claimed in claim 7, 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 supplys, the signal tune
It manages plate and communicates work(for realizing surface power supply, simulation power supply, unlock, boosting, activation, power switching control, AD acquisitions and ground bounce
Can, there is indicator light and button on the adapter panel；Test instruction that signal regulating panel sends out portable master station and
Testing process is exported to the electrical cabin of target missile or control cabinet, the test or integrated testability of the corresponding bay section of control target missile.
9. a kind of more running fire target missile control systems as claimed in claim 1 or 7, which is characterized in that further include telemetering console,
The telemetering console is sent it to for receiving the target missile state parameter that target missile flight course is passed down by wireless device
Emit operation console or portable master station, realizes the real-time monitoring and control to target missile state of flight.
10. a kind of more running fire target missile control systems as claimed in claim 7, which is characterized in that the portable master station is also
Including switch, button, indicator light, and convenient for the keyboard, display and mouse of human-computer interaction, the keyboard, display and mouse
Mark is connected by serial ports board with portable master station.
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