CN106205264A - A kind of guided missile rear test simulation training method and system - Google Patents
A kind of guided missile rear test simulation training method and system Download PDFInfo
- Publication number
- CN106205264A CN106205264A CN201610729361.9A CN201610729361A CN106205264A CN 106205264 A CN106205264 A CN 106205264A CN 201610729361 A CN201610729361 A CN 201610729361A CN 106205264 A CN106205264 A CN 106205264A
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- 238000004088 simulation Methods 0.000 title claims abstract description 40
- 238000012549 training Methods 0.000 title claims abstract description 33
- 238000012360 testing method Methods 0.000 title claims abstract description 31
- 238000000034 method Methods 0.000 title claims abstract description 10
- 230000005611 electricity Effects 0.000 claims description 5
- 238000012937 correction Methods 0.000 claims description 3
- 239000003054 catalyst Substances 0.000 claims 1
- 230000007423 decrease Effects 0.000 abstract description 2
- 238000005516 engineering process Methods 0.000 description 6
- 230000008901 benefit Effects 0.000 description 3
- 238000004364 calculation method Methods 0.000 description 1
- 230000036461 convulsion Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000005553 drilling Methods 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
Classifications
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- G—PHYSICS
- G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
- G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
- G09B9/00—Simulators for teaching or training purposes
- G09B9/003—Simulators for teaching or training purposes for military purposes and tactics
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- Theoretical Computer Science (AREA)
- Business, Economics & Management (AREA)
- Physics & Mathematics (AREA)
- Educational Administration (AREA)
- Educational Technology (AREA)
- General Physics & Mathematics (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The present invention relates to a kind of guided missile rear test simulation training method and system, including rear boiler-plate and tester simulation box, rear boiler-plate is internally provided with motor and distribution board, motor connects rudder sheet, and rudder sheet connects left restraint sensor, right restraint sensor and null pick-up；Tester simulation box includes microcomputer and control panel, and microcomputer connects control panel and sensor.The present invention uses cheap motor to simulate the scheme of steering wheel motion, decreases the cost of simulation training, constructs complete rear test simulation training system, blank in having filled up the army that this type of missile rear test simulation training cartridge is standby.
Description
Technical field
The present invention relates to military drilling simulation field, it particularly relates to a kind of guided missile rear test simulation training method
With system.
Background technology
The simulation training of modernization has become as the important component part of military training means.Since entering 21 century, meter
Calculation machine emulation technology, network technology and virtual reality technology achieve quickly development, provide important for analog simulation training
Technical support so that analog simulation training system with its distinctive verisimilitude, interactivity and economy, progressively replace reality dress
The standby new tool becoming information age military training.
In the training of guided missile rear test, actual load steering wheel is the active member of an electro-hydraulic mixing, is provided with again rudder electricity
Position meter provides rudder sheet location deflection angular dimension, and it can constitute a closed loop system together with rear tester.But use
Actual load steering wheel is simulated training, and cost is the highest, loses the meaning of simulation training.
Summary of the invention
The technical problem to be solved is that providing a kind of uses virtual closed loop control technology to carry out guided missile rear
The system and method for test simulation training.
Technical scheme can be realized by techniques below measure: a kind of guided missile rear test simulation training is
System, including: rear boiler-plate, tester simulation box, wherein,
Described rear boiler-plate is internally provided with motor and distribution board, and described motor connects rudder sheet, described
Connect on rudder sheet and have left restraint sensor, right restraint sensor and null pick-up；
Described tester simulation box includes microcomputer and control panel, and described microcomputer connects described chain of command
Plate and described left restraint sensor, right restraint sensor, null pick-up；
Described motor connects driver, and described driver connects described microcomputer.
Preferably, described distribution board includes A.C. contactor, earth leakage circuit-breaker, emergency stop switch and Switching Power Supply, and 12V is straight
Stream electricity output port, 220V alternating current output port；Described A.C. contactor connects civil power, and civil power is changed by described Switching Power Supply
For 12V unidirectional current and connect described 12V DC output end mouth, between described Switching Power Supply and A.C. contactor and described
Being respectively connected with earth leakage circuit-breaker between 220V alternating current output port and A.C. contactor, described A.C. contactor is also associated with
Emergency stop switch.
Preferably, described control panel is provided with potentiometer, toggle switch, voltmeter, ammeter, display lamp, number
Pipe and testing button.
Preferably, described microcomputer connects A/D converter and D/A converter, and described A/D converter connects described
Potentiometer and toggle switch, described D/A converter connects described voltmeter and ammeter.
Preferably, being provided with electrical equipment shelf inside described rear boiler-plate, described driver, distribution board are both placed in described electricity
On device shelf.
Preferably, the bottom of described rear boiler-plate is provided with support.
A kind of side using above-mentioned guided missile rear test simulation training system to carry out the test virtual closed loop control of guided missile tail end
Method, comprises the following steps:
A, uses the closed loop moving of the motor simulation actual load steering wheel that can perform opened loop control；
B, uses left restraint sensor, right restraint sensor and null pick-up that the operating of motor is carried out zero-bit inspection
Survey and position correction；
C, uses potentiometer to control the operation of motor；
D, gathers potentiometric output voltage and calculates rudder sheet deflection angle according to output voltage.
Compared with prior art, there is advantages that use virtual closed loop control technology, use price low
The motion of actual load steering wheel simulated by honest and clean motor, by whole flow processs of microcomputer simulation rear test, decreases
The cost of simulation training, constructs complete rear test simulation training system, has filled up guided missile rear test simulation training cartridge
In standby army, blank, has advance and novelty technically；Design science, rational in infrastructure weaponry simulation training lead
Territory occupies domestically leading level, is a scientific achievement with great military benefit and economic benefit.
Accompanying drawing explanation
The invention will be further described to utilize accompanying drawing, but the embodiment in accompanying drawing does not constitute any limit to the present invention
System.
Fig. 1 is the structural representation of the present invention a kind of guided missile rear test simulation training system.
Detailed description of the invention
For making the present invention easier to understand, the specific embodiment of the present invention is further illustrated below.
As it is shown in figure 1, a kind of guided missile rear test simulation training system, including: rear boiler-plate 1, tester simulation box
2, wherein,
Rear boiler-plate 1 is internally provided with four motors 3 and distribution board 4, and motor 3 connects rudder sheet 5, rudder sheet
Connect on 5 and have left restraint sensor 6, right restraint sensor 7 and null pick-up 8, left restraint sensor 6, right restraint sensor 7
It is Hall element with null pick-up 8；
Tester simulation box 2 is internal uses microcomputer 9 simulated interior circuit, controls motor 3 and simulates steering wheel
Motion under test status, microcomputer 9 connects control panel 10 and left restraint sensor 6, right restraint sensor 7, zero
Level sensor 8；
Motor 3 connects has driver 11, driver 11 to connect microcomputer 9.
Distribution board 4 includes A.C. contactor 12, earth leakage circuit-breaker 13, emergency stop switch 14 and Switching Power Supply 15,12V direct current
Electricity output port 16,220V alternating current output port 17；A.C. contactor 12 connects civil power, and civil power is converted to by Switching Power Supply 15
12V unidirectional current also connects 12V DC output end mouth 16, between Switching Power Supply 15 and A.C. contactor 12 and 220V alternating current
Being respectively connected with earth leakage circuit-breaker 13 between output port 17 and A.C. contactor 12, A.C. contactor 12 is also associated with jerk and opens
Close 14.The alternating current of 220V, 50Hz is needed owing to motor 3 drives, the DC voltage of miscellaneous equipment needs ± 12V, therefore
Need to use Switching Power Supply 15 that convert alternating current is become unidirectional current.A.C. contactor 12, earth leakage circuit-breaker 13 are used for protecting system
The safety of system circuit.
Be provided with on control panel 10 potentiometer, toggle switch, voltmeter, ammeter, display lamp, charactron and test by
Button.
Microcomputer 9 connects A/D converter and D/A converter, and A/D converter connects potentiometer and toggle switch,
D/A converter connects voltmeter and ammeter.
Rear boiler-plate 1 is internal is provided with electrical equipment shelf, and driver 11, distribution board 4 are both placed on electrical equipment shelf, it is simple to be
System is safeguarded.
The function of rear boiler-plate 1 includes: one, and rear structure and the steering wheel of simulating certain type guided missile in outward appearance and structure are surveyed
Action under examination state, therefore the outward appearance of rear boiler-plate 1 and structure set according to the ratio of 1:1 with the rear structure of certain type guided missile
Meter；Two, whole simulated training system carries out distribution, by distribution board 4, the civil power of input is transformed into the voltage required for system；
Three, accommodate and ensure whole system and the safety device of operator safety；Four, support whole rear boiler-plate 1 in applicable operation
Height, therefore the bottom at rear boiler-plate 1 arranges support, and the bearing height of support for being supported on applicable operator by nacelle
The height of member's operation.
A kind of side using above-mentioned guided missile rear test simulation training system to carry out the test virtual closed loop control of guided missile tail end
Method, comprises the following steps:
A, uses the motor 3 that can perform opened loop control to simulate the closed loop moving of actual load steering wheel；
B, uses left restraint sensor 6, right restraint sensor 7 and null pick-up 8 that the operating of motor 3 is carried out zero
Position detection and position correction；
C, uses potentiometer to control the operation of motor 3；
D, gathers potentiometric output voltage and calculates rudder sheet 5 deflection angle according to output voltage.
Last institute is it should be noted that, the present invention is only protected by above example in order to technical scheme to be described
Protecting the restriction of scope, although being explained in detail the present invention with reference to preferred embodiment, those of ordinary skill in the art should
Understand, technical scheme can be modified or equivalent, without deviating from the essence of technical solution of the present invention
And scope.
Claims (7)
1. a guided missile rear test simulation training system, it is characterised in that including: rear boiler-plate, tester simulation box, its
In,
Described rear boiler-plate is internally provided with motor and distribution board, and described motor connects rudder sheet, described rudder sheet
Upper connection has left restraint sensor, right restraint sensor and null pick-up；
Described tester simulation box includes microcomputer and control panel, described microcomputer connect described control panel and
Described left restraint sensor, right restraint sensor, null pick-up；
Described motor connects driver, and described driver connects described microcomputer.
Guided missile rear test simulation training system the most according to claim 1, it is characterised in that described distribution board includes handing over
Stream catalyst, earth leakage circuit-breaker, emergency stop switch and Switching Power Supply, 12V DC output end mouth, 220V alternating current outfan
Mouthful；Described A.C. contactor connects civil power, and civil power is converted to 12V unidirectional current and connects described 12V direct current by described Switching Power Supply
Electricity output port, between described Switching Power Supply and A.C. contactor and described 220V alternating current output port and A.C. contactor
Between be respectively connected with earth leakage circuit-breaker, described A.C. contactor is also associated with emergency stop switch.
Guided missile rear test simulation training system the most according to claim 1, it is characterised in that set on described control panel
It is equipped with potentiometer, toggle switch, voltmeter, ammeter, display lamp, charactron and testing button.
Guided missile rear test simulation training system the most according to claim 3, it is characterised in that described microcomputer is even
Being connected to A/D converter and D/A converter, described A/D converter connects described potentiometer and toggle switch, described D/A converter
Connect described voltmeter and ammeter.
Guided missile rear test simulation training system the most according to claim 1, it is characterised in that in described rear boiler-plate
Portion is provided with electrical equipment shelf, and described driver, distribution board are both placed on described electrical equipment shelf.
Guided missile rear test simulation training system the most according to claim 1, it is characterised in that described rear boiler-plate
Bottom is provided with support.
7. one kind uses guided missile rear test simulation training system as claimed in claim 1 to carry out the test of guided missile tail end virtual to close
The method that ring controls, it is characterised in that comprise the following steps:
A, uses the closed loop moving of the motor simulation actual load steering wheel that can perform opened loop control；
B, use left restraint sensor, right restraint sensor and null pick-up the operating of motor is carried out zero testing and
Position correction；
C, uses potentiometer to control the operation of motor；
D, gathers potentiometric output voltage and calculates rudder sheet deflection angle according to output voltage.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610729361.9A CN106205264A (en) | 2016-08-25 | 2016-08-25 | A kind of guided missile rear test simulation training method and system |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610729361.9A CN106205264A (en) | 2016-08-25 | 2016-08-25 | A kind of guided missile rear test simulation training method and system |
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| Publication Number | Publication Date |
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| CN106205264A true CN106205264A (en) | 2016-12-07 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201610729361.9A Pending CN106205264A (en) | 2016-08-25 | 2016-08-25 | A kind of guided missile rear test simulation training method and system |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113188382A (en) * | 2021-05-12 | 2021-07-30 | 中国人民解放军海军航空大学航空作战勤务学院 | Missile technology preparation simulation system |
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| JP2003167508A (en) * | 2001-11-30 | 2003-06-13 | Fujitsu Ltd | Flight training data collecting device and flight training data collecting and evaluating device |
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| CN205430104U (en) * | 2016-02-04 | 2016-08-03 | 中国航天空气动力技术研究院 | Four -channel digit steering engine control system |
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2016
- 2016-08-25 CN CN201610729361.9A patent/CN106205264A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4465464A (en) * | 1983-02-03 | 1984-08-14 | Schoenberg George R | Ballistic missile structure simulator |
| JP2003167508A (en) * | 2001-11-30 | 2003-06-13 | Fujitsu Ltd | Flight training data collecting device and flight training data collecting and evaluating device |
| CN2708232Y (en) * | 2004-06-16 | 2005-07-06 | 铁岭昌茂源科技开发有限公司 | Simulation cruise missile target drone |
| CN105474782B (en) * | 2009-10-30 | 2014-01-22 | 上海宇航系统工程研究所 | A kind of control method of aerospacecraft driver train |
| EP2381205B1 (en) * | 2010-04-23 | 2013-06-19 | MBDA Deutschland GmbH | Method for simulating a mission of an unmanned armed aerial vehicle |
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| CN205430104U (en) * | 2016-02-04 | 2016-08-03 | 中国航天空气动力技术研究院 | Four -channel digit steering engine control system |
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| 张启信等: "基于图形和半实物仿真的导弹测试训练模拟系统实现", 《2002系统仿真技术及其应用学术论文集（第四卷）》 * |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113188382A (en) * | 2021-05-12 | 2021-07-30 | 中国人民解放军海军航空大学航空作战勤务学院 | Missile technology preparation simulation system |
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| Date | Code | Title | Description |
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| C06 | Publication | ||
| PB01 | Publication | ||
| TA01 | Transfer of patent application right | ||
| TA01 | Transfer of patent application right |
Effective date of registration: 20181129 Address after: No. 88 Houbaoying Road, Qinhuai District, Nanjing City, Jiangsu Province Applicant after: ARMY ENGINEERING University OF PLA Address before: 430075 Mailbox No. 15-4, 42 Luyu East Road, Wuhan City, Hubei Province Applicant before: Cheng Xude |
|
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20161207 |