CN110060541A - A kind of aircraft navigation attitude equipment simulating training system - Google Patents
A kind of aircraft navigation attitude equipment simulating training system Download PDFInfo
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- CN110060541A CN110060541A CN201910420641.5A CN201910420641A CN110060541A CN 110060541 A CN110060541 A CN 110060541A CN 201910420641 A CN201910420641 A CN 201910420641A CN 110060541 A CN110060541 A CN 110060541A
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- 238000012549 training Methods 0.000 title claims abstract description 96
- 238000004088 simulation Methods 0.000 claims abstract description 42
- 230000010354 integration Effects 0.000 claims abstract description 22
- 238000004364 calculation method Methods 0.000 claims abstract description 13
- 239000002775 capsule Substances 0.000 claims abstract description 13
- 238000012544 monitoring process Methods 0.000 claims description 16
- 238000006243 chemical reaction Methods 0.000 claims description 12
- 230000005611 electricity Effects 0.000 claims description 7
- 230000015572 biosynthetic process Effects 0.000 claims 1
- 238000003786 synthesis reaction Methods 0.000 claims 1
- 230000000694 effects Effects 0.000 abstract description 4
- 239000000306 component Substances 0.000 description 8
- 238000000034 method Methods 0.000 description 5
- 230000005540 biological transmission Effects 0.000 description 4
- 238000010586 diagram Methods 0.000 description 4
- 238000012360 testing method Methods 0.000 description 4
- 238000001514 detection method Methods 0.000 description 3
- 239000008358 core component Substances 0.000 description 2
- 238000004132 cross linking Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000007689 inspection Methods 0.000 description 2
- 238000000926 separation method Methods 0.000 description 2
- 238000013024 troubleshooting Methods 0.000 description 2
- 230000004888 barrier function Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 239000004973 liquid crystal related substance Substances 0.000 description 1
- 230000013011 mating Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 238000000819 phase cycle Methods 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 230000001360 synchronised effect Effects 0.000 description 1
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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
- G09B9/02—Simulators for teaching or training purposes for teaching control of vehicles or other craft
- G09B9/08—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer
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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
- G09B9/02—Simulators for teaching or training purposes for teaching control of vehicles or other craft
- G09B9/08—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer
- G09B9/12—Motion systems for aircraft simulators
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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
- G09B9/02—Simulators for teaching or training purposes for teaching control of vehicles or other craft
- G09B9/08—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer
- G09B9/16—Ambient or aircraft conditions simulated or indicated by instrument or alarm
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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
- G09B9/02—Simulators for teaching or training purposes for teaching control of vehicles or other craft
- G09B9/08—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer
- G09B9/16—Ambient or aircraft conditions simulated or indicated by instrument or alarm
- G09B9/20—Simulation or indication of aircraft attitude
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Abstract
The invention discloses a kind of aircraft navigation attitude equipment simulating training systems, belong to navigation attitude analog machine technical field, it includes operation training platform and Training Control platform, the operation training platform includes simulation actual load and analog capsule cabin panel, the simulation actual load includes that full attitude integration gyro, magnetic course transmitter, group amplifier, magnetic heading corrected Calculation device, control box, relay box, course position indicator and horizon indicator, the analog capsule cabin panel include navigation attitude power switch and rapid coordination button；The Training Control platform includes main control computer, fault setting unit and power-supply system, the main control computer is connect with the control box, the main control computer is connect by the fault setting unit with the relay box, and the power-supply system is that the Training Control platform and the operation training platform are powered.Aircraft navigation attitude equipment simulating training system of the present invention, can simulate a variety of permanent faults, have the characteristics that training effect is good, training is at low cost.
Description
Technical field
The present invention relates to navigation attitude analog machine technical field, specifically a kind of aircraft navigation attitude equipment simulating training system.
Background technique
Aviation attitude system is important one of airborne equipment, mainly to measure, indicate the course angle and attitude angle of aircraft, and
Other equipment provide course and attitude reference on machine.At present due to not dedicated for the aviation attitude system training cartridge of Training for practice
It sets, universities and colleges rely primarily on aviation attitude system actual load and carry out teaching, major defect are as follows: first is that installing equipment is expensive, be trained to
This height；Second is that the operation of mistake is it is also possible to cause the damage of installing equipment during teaching and training；Third is that if using real
Dress is trained, and the phenomenon of the failure occurred in use can not reappear.
Publication No. is that the patent document of CN109733643A discloses a kind of aircraft navigation attitude device test system, belongs to aircraft
Navigation attitude technical field, the aircraft navigation attitude device test system include control system, power control unit, signal modulation unit and show
Show device, control system includes industrial personal computer and functional cards group, and display is connect by VGA line with the industrial personal computer, and industrial personal computer is logical
It crosses functional cards group to connect with signal modulation unit and tested aviation attitude system respectively, signal modulation unit and tested aviation attitude system connect
It connects, completes the processing to angular amount and discrete magnitude signal, realization outputs and inputs angular amount and discrete magnitude signal；Power supply control
Unit processed is connect with tested aviation attitude system, is protected for providing electric energy, Phase sequence detection to the tested aviation attitude system and providing power supply
Shield.Aircraft navigation attitude device test system structure is simple, compact to design, measuring accuracy is high, test content is comprehensive for this.But the Shen
Please be suitable for being tested for the property aviation attitude system and fault location, be not applied for low cost for the purpose of simulated training,
It is able to carry out the aircraft aviation attitude system simulated training of fault simulation reproduction.
Publication No. is that the patent document of 108897239 A of CN discloses a kind of spacecraft two-stage gesture stability simulation system,
For verifying the three hypervisor technologies such as spacecraft " superhigh precision direction ", " ultrastability control ", " super quick control ".Verifying
System includes: celestial body, load simulator, is actively directed toward platform, celestial body level-one control loop and load simulator Two-stage control time
Road；Celestial body level-one control loop and load simulator secondary control loop include: control unit, executing agency, measuring unit；
Celestial body level-one control loop is connected with load simulator secondary control loop by platform；Actively being directed toward platform is load simulator
Secondary control loop provides active controlling force；Load simulator passes through the reaction force biography for being actively directed toward platform for active controlling force
Pass celestial body level-one control loop.The spacecraft two-stage gesture stability simulation system of invention building, which can verify that, three surpasses platform space flight
Device multistage composite control technology and Control performance standard.But this application can not solve it is low for the purpose of simulated training
Cost is able to carry out the problem of aircraft aviation attitude system simulated training of fault simulation reproduction.
Summary of the invention
In view of this, the present invention is directed to the deficiency of existing actual load training, a kind of aircraft navigation attitude equipment simulating training system is designed
The performance detection training regular inspection and trained, the typical permanent fault of electrifying method of aircraft aviation attitude system may be implemented in system, the system
The functions such as simulation and troubleshooting training, meet the needs of universities and colleges carry out aviation attitude system teaching.
In order to solve the above technical problems, the technical solution used in the present invention is: a kind of aircraft navigation attitude equipment simulating training
System, including operation training platform and Training Control platform, the operation training platform includes simulating actual load and analog capsule cabin panel, described
Simulation actual load include full attitude integration gyro, magnetic course transmitter, group amplifier, magnetic heading corrected Calculation device, control box, after
Electrical appliance kit, course position indicator and horizon indicator, the analog capsule cabin panel include navigation attitude power switch and rapid coordination
Button；The Training Control platform includes main control computer, fault setting unit and power-supply system, the main control computer with it is described
Box connection is controlled, the main control computer is connect by the fault setting unit with the relay box, the power-supply system
It powers for the Training Control platform and the operation training platform.
Further, the magnetic course transmitter, the magnetic heading corrected Calculation device and the course position indicator according to
Secondary connection, the full attitude integration gyro, the group amplifier and the course position indicator are sequentially connected, the control
Box and the relay box are connect with the full attitude integration gyro, and the relay box and the full attitude integration gyro are equal
It is connect with the horizon indicator.
Further, the navigation attitude power switch controls the simulation actual load on/off, the rapid coordination button control
Make the simulation actual load circuit connection.
Further, the fault setting unit includes relay board and component access control interface, the master control meter
Calculation machine, the relay board, component access control interface and the relay box are sequentially connected.
Further, the power-supply system includes Power Supply Monitoring and power conversion, the three-phase alternating current of 36V/400Hz and
27V direct current is that the simulation actual load and the fault setting unit supply by the Power Supply Monitoring and the power conversion
Electricity.
Further, it is straight to pass through the Power Supply Monitoring for the three-phase alternating current of the 36V/400Hz and the 27V direct current
It is connected in the simulation actual load power supply, the 27V direct current is that the failure is set by the Power Supply Monitoring and the power conversion
The secondary power supply of unit offer+5V He+12V are provided.
Further, the relay board is by the PCL- based on PCI core bus that installs in the main control computer
The control of 722 boards.
Further, the main control computer is passed by the power supply circuit, signal of simulation actual load described in RS232 bus marco
Transmit electricity road, synchro system circuit, the imput output circuit of amplifier and relay box power supply and control circuit.
Compared with prior art, beneficial effects of the present invention are as follows:
Aircraft navigation attitude equipment simulating training system of the present invention, the simulation actual load include full attitude integration gyro, magnetic heading sensing
Device, group amplifier, magnetic heading corrected Calculation device, control box, relay box, course position indicator and horizon indicator, institute
Stating analog capsule cabin panel includes navigation attitude power switch and rapid coordination button, can carry out Comprehensive to aircraft aviation attitude system
Simulated training can guarantee training effect moreover, by the cooperation simulated training in operation training platform and Training Control platform
While, reduce cost；
Information, the fault setting list of the Training Control platform are transmitted between the operation training platform and the Training Control platform
Member, core component be relay board, relay board be stuck in main control computer driving under, control simulation actual load power supply electricity
Road, sensor circuit, transmission line, amplifier circuit, control box circuit, relay box circuit and indicator circuit, it is described after
Electric appliance board is using open circuit, short circuit and seals in the methods of resistance, simulation branch resistance variation, realizes navigation attitude separation unit and navigation attitude
The power supply trouble of system, combination gyro failure, Magnetic Sensor failure, transmission line failure, amplifier failures, control box failure,
The in-site modeling of relay box failure, indicator failure etc. 176 typical permanent faults, analog content is extensive, and training effect is good,
And it is able to carry out multiplicating training, meet the needs of universities and colleges carry out aviation attitude system teaching.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of operation of the present invention training station；
Fig. 2 is the structural schematic diagram of Training Control platform of the present invention；
Fig. 3 is circuit diagram of the invention；
Fig. 4 is the driving circuit figure of invention relay board；
Fig. 5 is the circuit diagram of invention power-supply system.
Specific embodiment
For a better understanding of the present invention, the contents of the present invention, but this hair are further fairly set out below with reference to embodiment
Bright protection content is not limited solely to the following examples.In the following description, give a large amount of concrete details so as to
More thorough understanding of the invention is provided.It will be apparent, however, to one skilled in the art that the present invention can be with
It is carried out without one or more of these details.
Embodiment one
As shown in Fig. 1 ~ 3, a kind of aircraft navigation attitude equipment simulating training system, including operation training platform and Training Control platform, it is described
Operation training platform includes simulation actual load and analog capsule cabin panel, and the simulation actual load includes full attitude integration gyro, magnetic heading biography
Sensor, group amplifier, magnetic heading corrected Calculation device, control box 3, relay box, course position indicator 2 and horizon indicator
1, the analog capsule cabin panel includes navigation attitude power switch 4 and rapid coordination button 5；The Training Control platform includes that master control calculates
Machine 6, fault setting unit and power-supply system, the main control computer are connect with the control box, and the main control computer passes through
The fault setting unit is connect with the relay box, and the power-supply system is the Training Control platform and the operation training
Platform power supply.
The magnetic course transmitter, the magnetic heading corrected Calculation device and the course position indicator 2 are sequentially connected, institute
It states full attitude integration gyro, the group amplifier and the course position indicator 2 to be sequentially connected, the control box and described
Relay box is connect with the full attitude integration gyro, and the relay box and the full attitude integration gyro are with described
Flat indicator 1 connects.
The navigation attitude power switch controls the simulation actual load on/off, and the rapid coordination button controls the simulation
Actual load circuit connection.
The pathfinder and the horizon indicator are disposed in parallel on the operation training platform, show course respectively
And Horizon, it is observed convenient for operator, the control box is that navigation attitude controls box, and for adjusting navigation attitude, the control box is arranged in institute
It states below pathfinder, convenient for operation.
The aircraft navigation attitude equipment simulating training system of the embodiment of the present invention, passes through the operation training platform and Training Control platform
Crosslinking simulate control, realize the performance detection training regular inspection and electrifying method training, typical permanent fault of aircraft aviation attitude system
Simulation and troubleshooting training etc. functions, meet universities and colleges carry out aviation attitude system teaching the needs of.
Embodiment two
As shown in Fig. 1 ~ 3, a kind of aircraft navigation attitude equipment simulating training system, including operation training platform and Training Control platform, it is described
Operation training platform includes simulation actual load and analog capsule cabin panel, and the simulation actual load includes full attitude integration gyro, magnetic heading biography
Sensor, group amplifier, magnetic heading corrected Calculation device, control box 3, relay box, course position indicator 2 and horizon indicator
1, the analog capsule cabin panel includes navigation attitude power switch 4 and rapid coordination button 5；The Training Control platform includes that master control calculates
Machine 6, fault setting unit and power-supply system, the main control computer are connect with the control box, and the main control computer passes through
The fault setting unit is connect with the relay box, and the power-supply system is the Training Control platform and the operation training
Platform power supply.
The magnetic course transmitter, the magnetic heading corrected Calculation device and the course position indicator 2 are sequentially connected, institute
It states full attitude integration gyro, the group amplifier and the course position indicator 2 to be sequentially connected, the control box and described
Relay box is connect with the full attitude integration gyro, and the relay box and the full attitude integration gyro are with described
Flat indicator 1 connects.
The navigation attitude power switch controls the simulation actual load on/off, and the rapid coordination button controls the simulation
Actual load circuit connection.
The aircraft navigation attitude equipment simulating training system of the embodiment of the present invention, with embodiment one the difference is that: it is described
Fault setting unit includes relay board and component access control interface, the main control computer, the relay board, institute
It states component access control interface and the relay box is sequentially connected.
The relay board is by the PCL-722 board control based on PCI core bus installed in the main control computer
System.
In the embodiment of the present invention, the fault setting unit, core component be relay board, relay board is stuck in
Under main control computer driving, power supply circuit, sensor circuit, transmission line, amplifier circuit, the control box of control simulation actual load
Circuit, relay box circuit and indicator circuit, the relay board is using open circuit, short circuit and seals in resistance, simulation branch
The methods of resistance variations realize power supply trouble, the combination gyro failure, Magnetic Sensor event of navigation attitude separation unit and aviation attitude system
176 typical case Chang Fa such as barrier, transmission line failure, amplifier failures, control box failure, relay box failure, indicator failure
The in-site modeling of failure, analog content is extensive, and training effect is good, and is able to carry out multiplicating training.
The fault setting unit passes through the switching and control of relay, realizes to each component of heading and attitude equipment crosslinking circuit
Open circuit, short circuit, resistance concatenation, to simulate the failure of aviation attitude system.Relay board is by the base installed in main control computer
It is controlled in the PCL-722 board of PCI core bus, PCL-722 is a overall length PCI board card, is divided into six main sides with 144 tunnels
I/O mouthfuls of programmable digital of mouth (CN0-CN5).Each port emulates the operation of the mode O of 8255 Programmable Peripheral Interfaces,
But it is capable of providing driving capability more higher than 8255.Each port is made of three 8 seat ports (A, B, C), they are TTL
Parallel interface provides three state buffer function when as input, provides data latch function when as output, can pass through
These three subports are arranged respectively to input or output port by software.The driving circuit of relay board is as shown in Figure 4.
The working principle of driving circuit are as follows: main control computer is by the I/O output port of PCL-722 board control logic
The input terminal of photoisolator is sent, to drive luminous tube, the output end of luminous tube exports level logic corresponding with input terminal,
Using the Darlington rp-drive ULN2803A of open collector, relay can be directly driven.When PCL-722 board exports
When data are 0, optocoupler conducting, output indicator is bright, relay actuation；When output data is 1, optocoupler is not turned on, output instruction
Lamp goes out, and relay board does not work.
Embodiment three
The aircraft navigation attitude equipment simulating training system of the embodiment of the present invention, with embodiment one, two the difference is that: the electricity
Source system includes Power Supply Monitoring 7 and power conversion, and the three-phase alternating current and 27V direct current of 36V/400Hz passes through the power supply
Monitoring 7 and the power conversion are that the simulation actual load and the fault setting unit are powered.
It is described that the three-phase alternating current of the 36V/400Hz and the 27V direct current, which pass through the Power Supply Monitoring directly,
Actual load power supply is simulated, the 27V direct current is that the fault setting unit mentions by the Power Supply Monitoring and the power conversion
For the secondary power supply of+5V and+12V.
In the embodiment of the present invention, the power-supply system is mainly the simulation actual load and the instruction of the operation training platform
The fault setting unit for practicing console provides power supply, wherein providing the three-phase alternating current of 36V/400Hz for the simulation actual load
Electricity and 27V direct current, provide the secondary power supply of+5V He+12V for the fault setting unit.Its internal relations figure such as Fig. 5 institute
Show.
Example IV
As shown in Fig. 1 ~ 3, a kind of aircraft navigation attitude equipment simulating training system, including operation training platform and Training Control platform, it is described
Operation training platform includes simulation actual load and analog capsule cabin panel, and the simulation actual load includes full attitude integration gyro, magnetic heading biography
Sensor, group amplifier, magnetic heading corrected Calculation device, control box 3, relay box, course position indicator 2 and horizon indicator
1, the analog capsule cabin panel includes navigation attitude power switch 4 and rapid coordination button 5；The Training Control platform includes that master control calculates
Machine 6, fault setting unit and power-supply system, the main control computer are connect with the control box, and the main control computer passes through
The fault setting unit is connect with the relay box, and the power-supply system is the Training Control platform and the operation training
Platform power supply.
The magnetic course transmitter, the magnetic heading corrected Calculation device and the course position indicator 2 are sequentially connected, institute
It states full attitude integration gyro, the group amplifier and the course position indicator 2 to be sequentially connected, the control box and described
Relay box is connect with the full attitude integration gyro, and the relay box and the full attitude integration gyro are with described
Flat indicator 1 connects.
The fault setting unit includes relay board and component access control interface, the main control computer, described
Relay board, component access control interface and the relay box are sequentially connected.
The relay board is by the PCL-722 board control based on PCI core bus installed in the main control computer
System.
The navigation attitude power switch controls the simulation actual load on/off, and the rapid coordination button controls the simulation
Actual load circuit connection.
The power-supply system includes Power Supply Monitoring and power conversion, and the three-phase alternating current and 27V direct current of 36V/400Hz is equal
It is that the simulation actual load and the fault setting unit are powered by the Power Supply Monitoring 7 and the power conversion.
It is described that the three-phase alternating current of the 36V/400Hz and the 27V direct current, which pass through the Power Supply Monitoring directly,
Actual load power supply is simulated, the 27V direct current is that the fault setting unit mentions by the Power Supply Monitoring and the power conversion
For the secondary power supply of+5V and+12V.
The aircraft navigation attitude equipment simulating training system of the embodiment of the present invention, exists with the difference of embodiment one, two, three
In: the main control computer 6 by the power supply circuit, signal circuit of simulation actual load described in RS232 bus marco, it is synchronous with
The power supply and control circuit of dynamic circuit system, the imput output circuit of amplifier and relay box.
The main control computer is the control centre of aviation attitude system simulated training, carry out system starting control, fault setting,
Magnificent 610H industrial control computer is ground in the operations such as training subject selection, system selection, and PCL-722 number I/O card is installed in inside, and
It is mating that mouse, keyboard, big viewing angle liquid crystal displays etc. are installed, actual load is simulated by software control, to simulate aviation attitude system
Function.
In the embodiment of the present invention, the main control computer of the Training Control platform controls analog component by RS232 bus
Power supply circuit, signal circuit, synchro system circuit, the imput output circuit of amplifier, relay box power supply and
The working environment as airborne aviation attitude system is simulated and created to control circuit, forces the use for training object operation more
Very.
Finally, it is stated that the above examples are only used to illustrate the technical scheme of the present invention and are not limiting, this field is common
Other modifications or equivalent replacement that technical staff makes technical solution of the present invention, without departing from technical solution of the present invention
Spirit and scope, be intended to be within the scope of the claims of the invention.
Claims (8)
1. a kind of aircraft navigation attitude equipment simulating training system, it is characterised in that: described including operation training platform and Training Control platform
Operation training platform includes simulation actual load and analog capsule cabin panel, and the simulation actual load includes full attitude integration gyro, magnetic heading biography
Sensor, group amplifier, magnetic heading corrected Calculation device, control box, relay box, course position indicator and horizon indicator,
The analog capsule cabin panel includes navigation attitude power switch and rapid coordination button；The Training Control platform include main control computer,
Fault setting unit and power-supply system, the main control computer are connect with the control box, and the main control computer passes through described
Fault setting unit is connect with the relay box, and the power-supply system is that the Training Control platform and the operation training platform supply
Electricity.
2. aircraft navigation attitude equipment simulating training system as described in claim 1, it is characterised in that: the magnetic course transmitter,
The magnetic heading corrected Calculation device and the course position indicator are sequentially connected, the full attitude integration gyro, the synthesis
Amplifier and the course position indicator are sequentially connected, the control box and the relay box with the full attitude integration
Gyro connection, the relay box and the full attitude integration gyro are connect with the horizon indicator.
3. aircraft navigation attitude equipment simulating training system as described in claim 1, it is characterised in that: the navigation attitude power switch control
The simulation actual load on/off is made, the rapid coordination button controls the simulation actual load circuit connection.
4. aircraft navigation attitude equipment simulating training system as described in claim 1, it is characterised in that: the fault setting unit packet
Include relay board and component access control interface, the main control computer, the relay board, component access control
Interface and the relay box are sequentially connected.
5. aircraft navigation attitude equipment simulating training system as described in claim 1, it is characterised in that: the power-supply system includes electricity
Source monitoring and power conversion, the three-phase alternating current and 27V direct current of 36V/400Hz pass through the Power Supply Monitoring and the power supply
It is transformed to the simulation actual load and fault setting unit power supply.
6. aircraft navigation attitude equipment simulating training system as claimed in claim 5, it is characterised in that: the three of the 36V/400Hz
Phase alternating current and the 27V direct current are directly that the simulation actual load is powered by the Power Supply Monitoring, the 27V direct current
The secondary power supply of+5V He+12V are provided by the Power Supply Monitoring and the power conversion for the fault setting unit.
7. aircraft navigation attitude equipment simulating training system as claimed in claim 4, it is characterised in that: the relay board is by institute
State the PCL-722 board control based on PCI core bus installed in main control computer.
8. aircraft navigation attitude equipment simulating training system as described in claim 1, it is characterised in that: the main control computer passes through
Simulated described in RS232 bus marco the power supply circuit of actual load, signal circuit, synchro system circuit, amplifier it is defeated
Enter the power supply and control circuit of output circuit and relay box.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
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| CN201910420641.5A CN110060541B (en) | 2019-05-20 | 2019-05-20 | Simulation training system for airplane navigation posture equipment |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201910420641.5A CN110060541B (en) | 2019-05-20 | 2019-05-20 | Simulation training system for airplane navigation posture equipment |
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| CN110060541B CN110060541B (en) | 2024-04-26 |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110444070A (en) * | 2019-08-05 | 2019-11-12 | 中国人民解放军陆军工程大学 | A kind of antiaircraft gun equipment simulation maintenance training device |
| CN112634696A (en) * | 2020-12-21 | 2021-04-09 | 贝壳技术有限公司 | Fault positioning practice method and device, electronic equipment and storage medium |
| CN114550561A (en) * | 2022-03-04 | 2022-05-27 | 石思群 | Electronic components analog circuit training synthesizes demonstration platform |
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