CN105867437A - Aiming control equivalent apparatus for simulating rocket platform prism photoelectric collimation loop - Google Patents

Aiming control equivalent apparatus for simulating rocket platform prism photoelectric collimation loop Download PDF

Info

Publication number
CN105867437A
CN105867437A CN201610208277.2A CN201610208277A CN105867437A CN 105867437 A CN105867437 A CN 105867437A CN 201610208277 A CN201610208277 A CN 201610208277A CN 105867437 A CN105867437 A CN 105867437A
Authority
CN
China
Prior art keywords
control
collimation
circuit
signal
platform
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
CN201610208277.2A
Other languages
Chinese (zh)
Other versions
CN105867437B (en
Inventor
何欢
孙煜
王岩
解英梅
王超
董彦维
范毅
麻广林
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
China Academy of Launch Vehicle Technology CALT
Beijing Institute of Space Launch Technology
Original Assignee
China Academy of Launch Vehicle Technology CALT
Beijing Institute of Space Launch Technology
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by China Academy of Launch Vehicle Technology CALT, Beijing Institute of Space Launch Technology filed Critical China Academy of Launch Vehicle Technology CALT
Priority to CN201610208277.2A priority Critical patent/CN105867437B/en
Publication of CN105867437A publication Critical patent/CN105867437A/en
Application granted granted Critical
Publication of CN105867437B publication Critical patent/CN105867437B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D3/00Control of position or direction
    • G05D3/12Control of position or direction using feedback
    • G05D3/20Control of position or direction using feedback using a digital comparing device
    • G05D3/203Control of position or direction using feedback using a digital comparing device using fine or coarse devices

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Management, Administration, Business Operations System, And Electronic Commerce (AREA)
  • Telescopes (AREA)

Abstract

The invention provides an aiming control equivalent apparatus for simulating a rocket platform prism photoelectric collimation loop, for the purpose of satisfying the demands for self-check of a ground aiming system and army operator simulation aiming training. The apparatus comprises a test lunch control equivalent device and a platform equivalent device, the test lunch control equivalent device is electrically connected with the platform equivalent device, the test lunch control equivalent device comprises a power strip, a control board and a display plate, the platform equivalent device comprises a driving board and an amplifier board, and the platform equivalent device is equivalent to a rocket platform prism, realizes scanning of a motor in a limiting scope of +/-15 degrees under the "scanning" signals of the aiming control equivalent apparatus and realizes platform closed-loop autocollimation under the control of collimation currents of an aiming controller.

Description

A kind of simulated rocket platform prism photoelectricity collimation loop take aim at control equivalent device
Technical field
The present invention relates to point technique and closed loop collimation controls technical field, more particularly, to a kind of simulated fire Arrow platform prism photoelectricity collimation loop take aim at control equivalent device.
Background technology
Azimuth aiming is aimed at loop feature by ground aiming part and rocket and forms.By in ground aiming system Photoelectronic collimating instrument and rocket aim at the prism collimation in loop, are delivered on arrow by the earth azimuth reference, thus complete Become to aim at flow process.Such as, needed rocket bearing position is adjusted before the transmitting of carrier rocket so that it is The direction that accurate alignment is to be launched, this is accomplished by the real-time measurement system of a set of precision, passes through azimuthal The location having measured orientation in real time of degree adjusts.
In existing aiming measurement system, many employing visual sight methods are carried out.This system includes corner cube prism, mark Bar instrument, two visual sight unit and two two-dimentional guide rails.Corner cube prism is horizontally arranged on rocket platform, mark Bar instrument is placed in the pole device fixing point after geodesic survey, and two two dimension guide rails are placed in respectively through too greatly Two-dimentional guide rail fixing point after measurement, three fixing points are point-blank;Two visual sight unit are respectively It is arranged on two two-dimentional guide rails.
When using visual sight method to carry out aiming measurement, the repeated multiple times two dimension guide rail that carries out is needed to translate and visual Aiming at and just can be allowed to run-home, cause the measurement time long, job step is loaded down with trivial details.This makes the rib of rocket platform The control operation of taking aim in mirror photoelectricity collimation loop requires high, to the operation skill of manipulator, consummate degree and psychology element Matter is all test greatly.And it practice, take aim at control training occasion and chance be very limited amount of.It addition, take aim at The links such as Barebone self-inspection before use and joint-trial are the most all necessary, but this detection and test cannot be also It is not suitable in actual scene application.Therefore, being badly in need of one can simulated rocket platform prism photoelectricity collimation loop Take aim at control equivalent device, the demand aiminged drill to meet ground sighting system self-inspection and army manipulator to emulate.
Summary of the invention
Emulating, in order to meet ground sighting system self-inspection and army manipulator, the demand aiminged drill, the application provides A kind of can simulated rocket platform prism photoelectricity collimation loop take aim at control equivalent device, including survey send out control simulator and Platform simulator, described survey send out control simulator electrically connecting platform simulator, described survey send out control simulator include Power panel, panel and display panel, described platform simulator includes driving plate and power board, wherein platform equivalence Device equivalence rocket platform prism, realizes motor ± 15 ° under " scanning " signal taking aim at control equivalent device and limits model Enclose interior scanning, under the control of aiming controller collimation electric current, realize platform closed loop auto-collimation.
Further, described panel includes CPU and communicating circuit, and wherein communicating circuit is with the side of RS-422 Formula completes the communication of azimuth value, sends " scanning ", " aiming ", " communication " signal, and receives " preparation Good ", " quick district ", " collimation electric current ", " zero-crossing pulse " signal, described display panel is by 8 seven segment digital tubes Forming with display driver chip, the data that described CPU will show are sent to display driver chip, and display drives Chip is by directly driving numeral method, the angle measurement data of display photoelectronic collimating instrument after the form decoding of regulation.
Further, described power panel is made up of the switch power module of 5V and 12V, the switch of described 12V Power module includes ambipolar ± 12V power supply, should ± 12V power supply includes the first+12V that combination with one another connects Switch power module and the switch power module of the second+12V, the switch power module of described first+12V Vout end connects+12V power supply, the GND end of the switch power module of described first+12V and described second+12V Switch power module Vout end connect and ground connection ,+the Vin of the switch power module of described first+12V Hold and be connected and be connected+24V power supply with the+Vin end of the switch power module of described second+12V, described first -Vin the end of the switch power module of+12V is connected with-Vin the end of the switch power module of described second+12V And connecting the GND end of+24V power supply, the GND end of the switch power module of described second+12V connects-12V electricity Source.
Further, described driving plate includes operational amplifier, and described operational amplifier is used for the closed loop of motor certainly Collimation.
Further, power board is made up of one piece of power amplifier chip, enters the control signal driving plate output Row power amplification is to drive electric machine rotation.
Further, take aim at control equivalent device described in be configured to include single system mode of operation and total system Working mould Formula, in both mode of operations, described in take aim at control equivalent device and photoelectronic collimating instrument, aiming controller composition is closed Ring controls loop, and under single system mode of operation, platform simulator is just put, and the light pipe of photoelectronic collimating instrument is Angle of depression state, for sighting system self-inspection;Under total system mode of operation, platform simulator hangs upside down in emulation arrow In, the light pipe of photoelectronic collimating instrument is elevation angle state, completes emulation for manipulator and aimings drill and system integration test.
Further, in described close loop control circuit, described survey is sent out control simulator and is taken aim at outside control equivalent device described Portion is connected with 24V power supply and aiming controller.
Further, described survey send out control simulator also include power-supply filter, on and off switch, panel-switch group and Panel leds group, wherein power-supply filter is connected with on and off switch, and on and off switch is connected with power panel, Described power panel includes that power module, described display panel include display driver circuit, and described panel also includes shake Swing circuit, RS422 drives isolation circuit, reset circuit, clock circuit and controls output circuit, described panel Switches set and described panel leds group connect the CPU of described panel respectively, and described panel-switch group will outward Instruction input described CPU, described CPU send condition indicative signal to described panel leds group in portion, described multiple Position circuit, oscillating circuit are all to the unidirectional output signal of described CPU, and described CPU is to described output control circuit list To output signal, described RS422 drive isolation circuit via described communicating circuit connect described CPU, described CPU, Described communicating circuit and described RS422 drive isolation circuit to be bi-directionally connected to each other, to realize the two-way of data signal Communication, described CPU is to described display panel uniaxially output signal.
Further, described communicating circuit is serial communication change-over circuit, and described close loop control circuit is PID Close loop control circuit.
Further, described platform simulator also includes that motor, wherein said driving plate, power board and electrode depend on Secondary connection also the most uniaxially transmits signal, and described motor is also to described driving plate output feedback signal, and passes through Described close loop control circuit realizes platform closed loop auto-collimation as follows: collimate zero signal and photoelectronic collimating instrument Output enforcement Angle Position feedback signal subtract each other after as collimation angle of deviation signal be output to aiming controller and PID close loop control circuit, described aiming controller and PID close loop control circuit output collimation current signal, should Collimation current signal is imported into survey and sends out control simulator, and control simulator output collimation voltage signal is sent out in described survey, should Collimation voltage signal is through correcting, by the speed measure feedback of described motor, the real time rate Voltage Feedback that unit obtains The correction of signal, it is thus achieved that collimation rate variance voltage, this collimation rate variance voltage is imported into described platform etc. Imitate device and described PID close loop control circuit, described platform simulator and described PID close loop control circuit and institute The signal of the speed measure feedback correction unit output stating motor is imported into described photoelectronic collimating instrument.
The invention have the benefit that
(1) this device can simulate arrow upper mounting plate, ground launch vehicle measurement, constitutes closed loop with Ground-Aiming-Equipment Loop, under single system mode of operation, tie surface sighting system can complete self-inspection;In total system mode of operation Under, it is inverted in emulating simulated rocket platform prism collimation closed-loop path in arrow, helps manipulator to complete emulation and aim at Training and system integration test, improve the aiming technical ability of manipulator.In order to enable the collimation of true simulated rocket platform prism Loop state, we use PID closed loop control methods to realize photoelectric auto-collimation.
(2) being applied in combination by analog closed-loop pid control algorithm and switch power module, it is achieved that giving In the case of fixed different step voltages, close loop negative feedback point deviation voltage is stable in 40mv, and speed is followed the tracks of steady State error is stable in 0.2V.
(3) be ensure that the stability of closed loop control tracking accuracy by the modular design of switch power module, produce The volume weight cost of product is also minimized.
(4) present invention is applied as self-checking equipment in ground aiming system, and as emulator Promoting the use of in multiple armies, the stability of product and practicality are fully examined and are verified.
Accompanying drawing explanation
Fig. 1 shows the outside schematic diagram of platform simulator.
Fig. 2 shows that control simulator outer interface schematic diagram is sent out in survey.
Fig. 3 shows bipolar power supply combinational circuit diagram.
Fig. 4 shows and takes aim at control equivalent device hardware composition schematic diagram.
Fig. 5 shows closed loop control algorithm flow chart.
Detailed description of the invention
Below in conjunction with accompanying drawing, technical scheme is described.
A kind of can simulated rocket platform prism photoelectricity collimation loop take aim at control equivalent device, including survey send out control a simulator With platform simulator, described survey send out control simulator electrically connecting platform simulator, described survey send out control simulator bag Including power panel, panel and display panel, described platform simulator includes driving plate and power board, wherein platform etc. Effect device equivalence rocket platform prism, realizes motor ± 15 ° under " scanning " signal taking aim at control equivalent device and limits In the range of scanning, aiming controller collimation electric current control under realize platform closed loop auto-collimation.Such as Fig. 1 Shown in, in terms of external structure, platform simulator includes prism 1, revolving body 2 and base 3.
Described panel includes CPU and communicating circuit, and wherein communicating circuit completes orientation in the way of RS-422 The communication of angle value, sends " scanning ", " aiming ", " communication " signal, and receive " being ready to ", " quick district ", " collimation electric current ", " zero-crossing pulse " signal, described display panel is to be driven core by 8 seven segment digital tubes and display Sheet forms, and the data that described CPU will show are sent to display driver chip, and display driver chip is by regulation Numeral method, the angle measurement data of display photoelectronic collimating instrument are directly driven after form decoding.Survey and send out outside control simulator Interface, portion is as shown in Figure 2.
Described power panel is made up of the switch power module of 5V and 12V, the switch power module bag of described 12V Include ambipolar ± 12V power supply.
In order to realize motor closed loop control, it is necessary to use have enough power ± bipolar power supply of 12V. Owing to linear power supply price is high, and taking up space as volume for embedded system is the most thick and heavy, we use same The switch power module of equal-specification, the most both can reduce cost, can meet again the requirement in space.But city On field ± switch power module of 12V is all with+12V for design main road ,-12V is design bypass, the most main If road unloaded or load little in the case of, bypass just cannot obtain enough power drive motor reversals, and this is also Close loop negative feedback point deviation and speed steady-state error when making motor reversal do not reach design requirement, taking aim on arrow Quasi-closed-loop path state cannot truly be simulated.So Con trolling index during in order to ensure motor positive and inverse is all Can meet design requirement, we use the switch power module modular design of two pieces of+12V, thus ensure positive and negative When turning, the power supply of motor is all independent of one another, does not interacts.
As shown in Figure 3, should ± 12V power supply includes the switch power module of the first+12V that combination with one another connects With the switch power module of the second+12V, the Vout end connection+12V of the switch power module of described first+12V The switch power module of power supply, the GND end of the switch power module of described first+12V and described second+12V Vout end connect and ground connection ,+Vin the end of the switch power module of described first+12V and described second+12V + Vin the end of switch power module be connected and connect+24V power supply, the switch power module of described first+12V -Vin end be connected with-Vin the end of the switch power module of described second+12V and connect+24V power supply GND end, the GND end of the switch power module of described second+12V connects-12V power supply.
Described driving plate includes operational amplifier, and described operational amplifier is for the closed loop auto-collimation of motor.
Power board is made up of one piece of power amplifier chip, and the control signal driving plate output is carried out power amplification To drive electric machine rotation.
Described take aim at control equivalent device be configured to include single system mode of operation and total system mode of operation, this two In kind of mode of operation, described in take aim at control equivalent device and constitute close loop control circuit with photoelectronic collimating instrument, aiming controller, And under single system mode of operation, platform simulator is just put, the light pipe of photoelectronic collimating instrument is angle of depression state, uses In sighting system self-inspection;Under total system mode of operation, platform simulator hangs upside down in emulation arrow, photoelectronic collimating The light pipe of instrument is elevation angle state, completes emulation for manipulator and aimings drill and system integration test.
In described close loop control circuit, described survey is sent out control simulator and is taken aim at control equivalent device outside and 24V described Power supply is connected with aiming controller.
Take aim at control equivalent device hardware detailed construction as shown in Figure 4.Described survey is sent out control simulator and is also included power filter Device, on and off switch, panel-switch group and panel leds group, wherein power-supply filter is connected with on and off switch, On and off switch is connected with power panel, and described power panel includes that power module, described display panel include that display drives Circuit, described panel also includes that oscillating circuit, RS422 drive isolation circuit, reset circuit, clock circuit And control output circuit, described panel-switch group and described panel leds group connect described panel respectively CPU, and external command inputs described CPU by described panel-switch group, described CPU is to described panel leds Group sends condition indicative signal, and described reset circuit, oscillating circuit are all to the unidirectional output signal of described CPU, institute State CPU to lead to via described to the unidirectional output signal of described output control circuit, described RS422 driving isolation circuit News circuit connects described CPU, described CPU, described communicating circuit and described RS422 and drives isolation circuit each other Being bi-directionally connected, to realize the two-way communication of data signal, described CPU is to described display panel uniaxially output signal.
Described communicating circuit is serial communication change-over circuit, and described close loop control circuit is that PID closed loop control is returned Road.
Described platform simulator also includes that motor, wherein said driving plate, power board and electrode are sequentially connected with and depend on Sequence uniaxially transmits signal, and described motor is also to described driving plate output feedback signal, and by described closed loop control Loop processed realizes platform closed loop auto-collimation as follows: collimate the enforcement of zero signal and the output of photoelectronic collimating instrument Angle Position feedback signal is output to aiming controller and PID closed loop control as collimation angle of deviation signal after subtracting each other Loop processed, described aiming controller and PID close loop control circuit output collimation current signal, this collimation electric current is believed Number being imported into survey and send out a control simulator, control simulator output collimation voltage signal is sent out in described survey, and this collimation voltage is believed Number process corrects the correction of the real time rate voltage feedback signal that unit obtains by the speed measure feedback of described motor, Obtaining collimation rate variance voltage, this collimation rate variance voltage is imported into described platform simulator and described PID close loop control circuit, described platform simulator and described PID close loop control circuit and the survey of described motor The signal of speed feedback compensation unit output is imported into described photoelectronic collimating instrument.The flow process of above-mentioned feedback signal such as figure Shown in 5.
Although describing the present invention with reference to specific embodiment, it will be understood by those skilled in the art that can be not Carry out various change on the basis of departing from the scope of the invention or carry out equivalence replacement.It addition, can be without departing from this On the basis of bright scope, the content that present invention teach that is carried out various adjustment thus adapt to specific environment or material. Therefore, the present invention should not necessarily be limited by disclosed specific embodiment, but should include belonging to scope All embodiments.

Claims (10)

1. one kind can simulated rocket platform prism photoelectricity collimation loop take aim at control equivalent device, it is characterised in that Sending out control simulator and platform simulator including surveying, control simulator electrically connecting platform simulator, institute are sent out in described survey State survey control simulator and include that power panel, panel and display panel, described platform simulator include driving plate and merit Put plate, wherein platform simulator equivalence rocket platform prism, real under " scanning " signal taking aim at control equivalent device Scanning in the range of the restriction of existing motor ± 15 °, realizes platform closed loop under the control of aiming controller collimation electric current Auto-collimation.
The most according to claim 1 take aim at control equivalent device, it is characterised in that described panel includes CPU And communicating circuit, wherein communicating circuit completes the communication of azimuth value in the way of RS-422, send " scanning ", " aim at ", " communication " signal, and receive " being ready to ", " quick district ", " collimation electric current ", " zero-crossing pulse " Signal, described display panel is made up of 8 seven segment digital tubes and display driver chip, and described CPU will show Data be sent to display driver chip, display driver chip by regulation form decoding after directly drive charactron Display, the angle measurement data of display photoelectronic collimating instrument.
The most according to claim 2 take aim at control equivalent device, it is characterised in that described power panel is by 5V Forming with the switch power module of 12V, the switch power module of described 12V includes ambipolar ± 12V power supply, Should ± 12V power supply includes switch power module and the switch of the second+12V of the first+12V that combination with one another connects Power module, the Vout end of the switch power module of described first+12V connects+12V power supply, described first+12V The GND end of switch power module be connected with the Vout end of the switch power module of described second+12V and connect The switch power module of the ground ,+Vin end of the switch power module of described first+12V and described second+12V + Vin end is connected and connects+24V power supply ,-Vin the end of the switch power module of described first+12V and described -Vin the end of the switch power module of two+12V is connected and connects the GND end of+24V power supply, and described second The GND end of the switch power module of+12V connects-12V power supply.
The most according to claim 3 take aim at control equivalent device, it is characterised in that described driving plate includes fortune Calculating amplifier, described operational amplifier is for the closed loop auto-collimation of motor.
The most according to claim 4 take aim at control equivalent device, it is characterised in that power board is by one piece of merit Rate amplification chip forms, and the control signal driving plate output is carried out power amplification to drive electric machine rotation.
The most according to claim 5 take aim at control equivalent device, it is characterised in that described in take aim at control equivalent device Be configured to include single system mode of operation and total system mode of operation, in both mode of operations, described in take aim at Control equivalent device constitutes close loop control circuit with photoelectronic collimating instrument, aiming controller, and at single system Working mould Under formula, platform simulator is just put, and the light pipe of photoelectronic collimating instrument is angle of depression state, for sighting system self-inspection;? Under total system mode of operation, platform simulator hangs upside down in emulation arrow, and the light pipe of photoelectronic collimating instrument is elevation angle state, Complete emulation for manipulator to aiming drill and system integration test.
The most according to claim 6 take aim at control equivalent device, it is characterised in that described close loop control circuit In, described survey is sent out control simulator and is taken aim at control equivalent device outside and 24V power supply and aiming controller phase described Connect.
The most according to claim 7 take aim at control equivalent device, it is characterised in that control simulator is sent out in described survey Also include power-supply filter, on and off switch, panel-switch group and panel leds group, wherein power-supply filter with On and off switch is connected, and on and off switch is connected with power panel, and described power panel includes power module, described aobvious Show that plate includes that display driver circuit, described panel also include that oscillating circuit, RS422 drive isolation circuit, answer Position circuit, clock circuit and control output circuit, described panel-switch group and described panel leds group connect respectively Meet the CPU of described panel, and described panel-switch group external command is inputted described CPU, described CPU to Described panel leds group sends condition indicative signal, and described reset circuit, oscillating circuit are all to described CPU Unidirectional output signal, described CPU to the unidirectional output signal of described output control circuit, described RS422 drive every Described CPU, described CPU, described communicating circuit and described RS422 is connected via described communicating circuit from circuit Driving isolation circuit to be bi-directionally connected to each other, to realize the two-way communication of data signal, described CPU is to described display Plate uniaxially output signal.
The most according to claim 8 take aim at control equivalent device, it is characterised in that described communicating circuit is string Row communication switching circuit, and described close loop control circuit is PID close loop control circuit.
The most according to claim 9 take aim at control equivalent device, it is characterised in that described platform simulator is also Including motor, wherein said driving plate, power board and electrode is sequentially connected with and the most uniaxially transmits signal, institute State motor also to described driving plate output feedback signal, and realized as follows by described close loop control circuit Platform closed loop auto-collimation: after the enforcement Angle Position feedback signal that collimation zero signal and photoelectronic collimating instrument export is subtracted each other It is output to aiming controller and PID close loop control circuit, described aiming controller as collimation angle of deviation signal With PID close loop control circuit output collimation current signal, this collimation current signal is imported into survey and sends out control equivalence Device, described survey sends out control simulator output collimation voltage signal, and this collimation voltage signal is through by described motor The correction of the real time rate voltage feedback signal that speed measure feedback correction unit obtains, it is thus achieved that collimation rate variance electricity Pressure, this collimation rate variance voltage is imported into described platform simulator and described PID close loop control circuit, institute State the speed measure feedback correction unit of platform simulator and described PID close loop control circuit and described motor The signal of output is imported into described photoelectronic collimating instrument.
CN201610208277.2A 2016-04-06 2016-04-06 Take aim at control equivalent device in a kind of simulated rocket platform prism photoelectricity collimation circuit Active CN105867437B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610208277.2A CN105867437B (en) 2016-04-06 2016-04-06 Take aim at control equivalent device in a kind of simulated rocket platform prism photoelectricity collimation circuit

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610208277.2A CN105867437B (en) 2016-04-06 2016-04-06 Take aim at control equivalent device in a kind of simulated rocket platform prism photoelectricity collimation circuit

Publications (2)

Publication Number Publication Date
CN105867437A true CN105867437A (en) 2016-08-17
CN105867437B CN105867437B (en) 2019-04-05

Family

ID=56628235

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610208277.2A Active CN105867437B (en) 2016-04-06 2016-04-06 Take aim at control equivalent device in a kind of simulated rocket platform prism photoelectricity collimation circuit

Country Status (1)

Country Link
CN (1) CN105867437B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109379583A (en) * 2018-11-26 2019-02-22 中国人民解放军陆军工程大学 A kind of portable television angular instrument device for fast detecting

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101140468A (en) * 2007-10-11 2008-03-12 中国科学院长春光学精密机械与物理研究所 Emulation test method of aerospace optical remote sensing machine focusing control circuit
CN201918631U (en) * 2010-11-29 2011-08-03 深圳市大族激光科技股份有限公司 Optical fiber laser
CN103792952A (en) * 2014-01-23 2014-05-14 中国科学院长春光学精密机械与物理研究所 Fast reflector electric control system for improving pointing accuracy of laser emission system
CN104714428A (en) * 2015-01-09 2015-06-17 西安应用光学研究所 Powering-up protection control circuit for photoelectric tracking instrument

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101140468A (en) * 2007-10-11 2008-03-12 中国科学院长春光学精密机械与物理研究所 Emulation test method of aerospace optical remote sensing machine focusing control circuit
CN201918631U (en) * 2010-11-29 2011-08-03 深圳市大族激光科技股份有限公司 Optical fiber laser
CN103792952A (en) * 2014-01-23 2014-05-14 中国科学院长春光学精密机械与物理研究所 Fast reflector electric control system for improving pointing accuracy of laser emission system
CN104714428A (en) * 2015-01-09 2015-06-17 西安应用光学研究所 Powering-up protection control circuit for photoelectric tracking instrument

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
孙左江: "某飞行器测试发射仿真训练系统设计与实现", 《中国优秀硕士学位论文全文数据库》 *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109379583A (en) * 2018-11-26 2019-02-22 中国人民解放军陆军工程大学 A kind of portable television angular instrument device for fast detecting

Also Published As

Publication number Publication date
CN105867437B (en) 2019-04-05

Similar Documents

Publication Publication Date Title
CN109062115B (en) Rolling ball control method based on double closed-loop control
CN102589531B (en) Underwater topography measurement boat as well as manufacturing method and measurement method
US2471315A (en) Aircraft trainer for aerial gunners
CN101382805B (en) Rate gyro stabilizing platform type antenna followup system
CN105737847B (en) The pilot system of closed loop independent navigation under the conditions of noncooperative target
CN102023643B (en) 3-PRP planar three-degree-of-freedom parallel mechanism positioning method
CN103353310A (en) Laser strapdown inertial navigation system
CN102706361A (en) Attitude precision estimation method of multiple high-accuracy inertial navigations system
CN109032041B (en) Rolling ball control system based on camera position detection
CN109631826A (en) A kind of satellite automated accuracy checking method
CN103674067A (en) Auto-collimation theodolite based transfer alignment verification method
CN105867437A (en) Aiming control equivalent apparatus for simulating rocket platform prism photoelectric collimation loop
CN203966431U (en) The target detection of a kind of dexterous ammunition device and control analogue system
CN107244431B (en) Space tasks ground motion reproduces across scale verification platform
CN102310953B (en) Portable earth simulator
Sushchenko Features of control of tracking modes
CN103529693B (en) A kind of hard rod control system
CN205262456U (en) Measurement device for space angle in jumbo size space
US2887873A (en) Method of measuring and compensating for deviation errors in earth's field sensitivedirection indicators
CN105512491A (en) Calibration method of fitting curve of attack angle and output voltage corresponding to attack angle
CN106155141A (en) Improve the rotating platform control system of turntable robustness and the adjustment method based on this system
CN112346358B (en) Semi-physical performance evaluation method and system of photoelectric search tracking system
CN208000499U (en) It is originated from main tracing system based on four-axle aircraft three dimensions plume
Murphy et al. EduCube: The 1U Educational CubeSat
CN109029497B (en) Mechanical navigation frame system for simulating space position of fixed star

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant