CN206115770U - Aircraft flight analogue test device - Google Patents
Aircraft flight analogue test device Download PDFInfo
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- CN206115770U CN206115770U CN201620515037.2U CN201620515037U CN206115770U CN 206115770 U CN206115770 U CN 206115770U CN 201620515037 U CN201620515037 U CN 201620515037U CN 206115770 U CN206115770 U CN 206115770U
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Abstract
The utility model discloses an aircraft flight analogue test device relates to aircraft test technical field. Aircraft flight analogue test device contains: main flight simulator, composite control manager, manipulation load unit, moving system unit, interface unit, avionics emulation ware, simulation passenger cabin, scene simulation unit, sound analogue unit, environment and support unit, still contain the real -time network unit for real -time data's exchange and communication between each modular unit of the aforesaid of control completion aircraft flight in -process. The utility model has the advantages of: can accomplish the aircraft flight process simulation, flight analysis of the data aassessment, control load device emulation, the emulation of instantaneous overload sensation, the emulation of avionics display and control system, smog is surveyed with report an emergency and ask for help or increased vigilance emulation, has fine practical value to flight performance, handling quality, control rule and the task envelope curve of research aircraft, makes the pilot know the flight characteristics and the driving technology of aircraft, the development process of aircraft with higher speed as early as possible.
Description
Technical field
The utility model is related to plane simulation experimental technique field, and in particular to a kind of aircraft flight simulation experimental rig.
Background technology
With developing rapidly for aeronautical technology and being continuously increased for aircraft system complexity, flight simulation test device
Indispensable important tool in modern aircraft design is become.Because flight simulation has more real motion feedback and psychology
Environment, it is ground flying simulation and the desired transition between real aircraft is taken a flight test.Developed country while research ＆ development in flight all
The huge financial resources of input of not stinting build each model flight simulation test device, using the flight simulation test device, to being related to fly
The advanced technology of machine design, such as design of control law technology, man-machine complex experimental technique and failure analysis techniques are carried out deeply
Research.L-G simulation test environment of this comprehensive people of flight simulation test device in loop has become and wind tunnel test environment, spray
The big experimental study facility of gas block testing stand, structural environment testing equipment aviation four arranged side by side.Flight simulation test device exists
Application in Domestic Aircraft Project R＆D relatively lags behind.Due to there is no flight simulation test device, in flight control system and electricity
Before subsystem hardware is developed, it is impossible to enter simulation study of the pedestrian in loop, pilot cannot early intervene aircraft development,
Project planner can not completely understand the manipulation demand of pilot, have impact on airplane design level, delay the lead time,
Also so that increased development cost because software and hardware is changed in a large number with cycle delay.
Utility model content
The purpose of this utility model is to provide a kind of aircraft flight simulation experimental rig, to solve or at least mitigate background skill
The problem at least one in the presence of art.
The technical solution of the utility model is：A kind of aircraft flight simulation experimental rig is provided, comprising main flight simulator,
Comprehensive control management device, manipulation load cell, kinematic system unit, interface unit, avionics system simulator, analog capsule cabin, what comes into a driver's are imitated
True unit, speech simulation unit, environment and supporter, real-time network unit；The main flight simulator is completed for control
The flight course emulation of aircraft；The comprehensive control management device is used for task scheduling and management and the flight that control completes aircraft
The analysis and evaluation of data；The load cell that manipulates is used for the manipulation load device emulation that control completes aircraft；The kinetic system
System unit is used for the instantaneous overload sensation emulation that control completes aircraft；The interface unit is used to complete the letter of aircraft cockpit equipment
Number collection, process and hardware board driving；The avionics system simulator is used to complete the avionics display ＆ control system emulation of aircraft；Institute
Analog capsule cabin is stated for completing the passenger cabin operating environment real-time simulation of aircraft；The vision simulation unit is used to complete the cabin of aircraft
Outer scene simulation；The speech simulation unit is used for various environment sound equipments emulation that control completes flight course；The environment with
Supporter completes power supply management, air conditioner ventilation and smoke detection with alarm emulation for control；The real-time network unit
The exchange of real time data and communication between each modular unit in aircraft flight are completed for control.
Preferably, flight course simulation package flight simulation and flight envelope side within flight envelope containing aircraft
The flight simulation on boundary, and the simulation of quantitative or qualitative simulation can be carried out to the failure occurred in flight course.
Preferably, the task scheduling sets with the analysis and evaluation of management and flying quality comprising test, topic of taking a flight test
Put；Flight environment of vehicle, airport condition Initialize installation；The setting of airplane fault and special circumstances；Flight course is monitored；Flying quality
Record, playback and analysis and evaluation.
Preferably, the manipulation load device simulation package contains under different flying conditions and different operating pattern lower-pilot systems
Static and dynamic c haracteristics simulation, to pilot provide drive actual airplane when manipulation force feeling.
Preferably, the instantaneous overload feels simulation package containing aircraft longitudinal direction, lifting, lateral, pitching, roll and course six
Free degree kinetic characteristic is simulated, and contact to earth to taking off, landing, stall is buffeted the dynamic of process and is simulated.
Preferably, the avionics display ＆ control system simulation package show, control, navigating containing the avionics related to flight, communicate with
And alarm function simulation.
Preferably, passenger cabin operating environment real-time simulation includes aircraft cockpit nacelle, seat, front panel, front control
The true simulation of making sheet, center console, left and right console and cockpit equipment.
Preferably, visual effect of the scene out of my cabin simulation comprising different flight state under various meteorological conditions and many
Plant the real-time simulation of natural scene and its relative motion dynamic effect.
Preferably, various environment sound equipment simulation packages containing the engine operating sound sent in aircraft flight, rise
Thunder, the patter of rain that frame folding and unfolding sound, alarm sound and the external environment of falling sends.
The utility model has the advantage of：Aircraft flight simulation experimental rig of the present utility model includes multiple modules, can
Feel imitative to complete the flight course emulation of aircraft, the analysis and evaluation of flying quality, manipulate load device emulation, instantaneous overload
Very, the emulation of avionics display ＆ control system, passenger cabin operating environment real-time simulation, out of my cabin scene simulation, environment sound equipment emulation, smoke detection with
Alarm emulation, the flying quality, handling quality, control law and task envelope curve to research aircraft has good practical value, makes
The flight characteristics and driving technology of pilot's Aircraft Familiarization as early as possible, greatly strengthens first-fly unit confidence, it is ensured that first-fly safe flight,
Accelerate the development process of aircraft type.
Description of the drawings
Fig. 1 is the schematic diagram of the aircraft flight simulation experimental rig of the embodiment of the utility model one.
Wherein, the main flight simulators of 1-, 2- comprehensive control management devices, 3- manipulates load cell, 4- kinematic system units, 5-
Interface unit, 6- avionics system simulators, 7- analog capsule cabins, 8- vision simulation units, 9- speech simulation units, 10- environment and support
Unit, 11- real-time network units, the main flight simulation computers of 101-, 201- console stage bodies, 202- control management computer,
203- record analyses show that computer, 301- manipulate load motor, 302- control links mechanism, 401- six-freedom motion machines
Structure, 402- manipulation/motion simulation computers, 501- interface computers, 502- analog input cards, 601- avionics simulation computers,
602- avionics display panel controls, 701- nacelles, 702- passenger cabin platforms, 703- cockpit equipments, 704- passenger cabins electrically and lighting unit,
801- vision simulation computers, 802- projectors, 803- show ball curtain, 901- sound simulation computers, 902- power amplifiers, 903- ears
Machine, 1001- power management units, 1002- air-conditioner ventilation units, 1003- smoke detection Alarm Units, 1101- real-time networks are handed over
Change planes, 1102- reflective memory cards.
Specific embodiment
Purpose, technical scheme and advantage to implement the utility model is clearer, below in conjunction with the utility model
Accompanying drawing in embodiment, is further described in more detail to the technical scheme in the utility model embodiment.In the accompanying drawings, ad initio
Same or similar element is represented to same or similar label eventually or the element with same or like function.Described reality
It is a part of embodiment of the utility model to apply example, rather than the embodiment of whole.Below with reference to the embodiment of Description of Drawings
It is exemplary, it is intended to for explaining the utility model, and it is not intended that to restriction of the present utility model.It is new based on this practicality
Embodiment in type, the every other enforcement that those of ordinary skill in the art are obtained under the premise of creative work is not made
Example, belongs to the scope of the utility model protection.Embodiment of the present utility model is described in detail below in conjunction with the accompanying drawings.
In description of the present utility model, it is to be understood that term " " center ", " longitudinal direction ", " horizontal ", "front", "rear",
The orientation or position relationship of the instruction such as "left", "right", " vertical ", " level ", " top ", " bottom " " interior ", " outward " is based on accompanying drawing institute
The orientation for showing or position relationship, are for only for ease of description the utility model and simplify description, rather than indicate or imply indication
Device or element must have specific orientation, with specific azimuth configuration and operation, therefore it is not intended that to this practicality
The restriction of novel protected scope.
As shown in figure 1, a kind of aircraft flight simulation experimental rig, comprising main flight simulator 1, comprehensive control management device 2,
Manipulate load cell 3, kinematic system unit 4, interface unit 5, avionics system simulator 6, analog capsule cabin 7, vision simulation unit 8, sound
Sound analogue unit 9, environment and supporter 10, above-mentioned each unit is connected with real-time network unit 11, real-time network unit 11
The exchange of real time data and communication between each modular unit in aircraft flight are completed for control.
In the present embodiment, main flight simulator 1 includes main flight simulation computer 101, and comprehensive control management device 2 is included
Console stage body 201, control management computer 202, record analysis show computer 203, manipulate load cell 3 negative comprising manipulating
Charged machine 301, control link mechanism 302, kinematic system unit 4 includes six-freedom motion mechanism 401, manipulation/motion simulation
Computer 402, interface unit 5 includes interface computer 501, analog input card 502, and avionics system simulator 6 includes avionics simulation calculation
Machine 601, avionics display panel control 602, analog capsule cabin 7 comprising nacelle 701, passenger cabin platform 702, cockpit equipment 703, passenger cabin electrically and
Lighting unit 704, vision simulation unit 8 includes vision simulation computer 801, projector 802, display ball curtain 803, speech simulation
Unit 9 includes sound simulation computer 901, power amplifier 902, earphone 903, and environment includes power management unit with supporter 10
1001st, air-conditioner ventilation unit 1002, smoke detection Alarm Unit 1003, real-time network unit 11 includes real-time network switch
1101st, reflective memory card 1102.
Main flight simulator 1 is used for the flight course emulation that control completes aircraft；In the present embodiment, main flight simulation meter
Calculation machine 101 is realized by the way of " the real-time flight simulation environment+reflective memory card based on RTX ".Main flight simulation computer
The initialization information of 101 real-time receptions control management computer 202 and the aircraft handling of manipulation/motion simulation computer 402
Information, obtains the state of flight of aircraft after real-time resolving, then by real-time network unit 11 by the state of flight of aircraft
Information is sent respectively to record analysis and shows computer 203, avionics simulation computer 601, vision simulation computer 801 and sound
Sound simulation computer 901.
Main flight simulation computer 101 runs main flight simulation software, number of the main flight simulation software according to record
Include the elements such as aircraft, runway, landform, sky, instrument, flight path, two-dimentional word, weather, special efficacy and chart according to generating one
Simulation figure environment, so as to simulate state of flight during Live Flying, such as simulated flight performance and fly control, engine,
Fall the systems such as frame.Additionally, the system is also provided navigating on data processing, parameter curve drafting, runway and terrain generation and chart
The miscellaneous functions such as mark Overlapping display.
In the present embodiment, flight course simulation package flight simulation and flight envelope within flight envelope containing aircraft
The flight simulation on border, and the simulation of quantitative or qualitative simulation can be carried out to the failure occurred in flight course.
Comprehensive control management device 2 is used for control to be completed the task scheduling of aircraft and manages and the analysis of flying quality is commented
Estimate；In the present embodiment, console stage body 201 adopts 19U standard cabinets；Control management computer 202 and record analysis show
Computer 203 is respectively adopted the mode of " industrial computer+reflective memory card " and realizes, runs different simulation softwares；Control management meter
Calculation machine 202 is responsible for completing the scheduling of aerial mission, management and control；Record analysis shows that computer 203 is responsible for completing flight number
According to record, playback, show in real time and flight quality assessment.
In the present embodiment, task scheduling includes test, topic of taking a flight test with the analysis and evaluation of management and flying quality
Arrange；Flight environment of vehicle, airport condition Initialize installation；The setting of airplane fault and special circumstances；Flight course is monitored；Flight number
According to record, playback and analysis and evaluation.
Manipulating load cell 3 is used for the manipulation load device emulation that control completes aircraft；In the present embodiment, load is manipulated
Motor 301 is linked together using triple channel electric loading system device with nacelle 701 and passenger cabin platform 702；Control link mechanism 302
It is responsible for completing the connection of cabin control mechanism and electric loading system device.
In the present embodiment, manipulate under load device simulation package flying conditions containing difference and different operating pattern lower-pilot systems
The static and dynamic c haracteristics simulation of system, to pilot manipulation force feeling when driving actual airplane is provided.
Kinematic system unit 4 is used for the instantaneous overload sensation emulation that control completes aircraft；In the present embodiment, six degree of freedom
Motion 401 is realized using electronic mode, linked together with nacelle 701 and passenger cabin platform 702, is responsible for completing the six of aircraft
Free movement is simulated；Manipulation/motion simulation computer 402 is realized by the way of " industrial computer+reflective memory card ", is responsible for completing
The calculating of load force and the resolving of Motion Controlling Model are manipulated, it exists two-way between main flight simulation computer 101
Information transfering relation.
In the present embodiment, instantaneous overload feels simulation package containing aircraft longitudinal direction, lifting, lateral, pitching, roll and course
Six-freedom motion simulated behavior, and contact to earth to taking off, landing, the dynamic simulation of process is buffeted in stall.
Interface unit 5 is used to complete the signals collecting of aircraft cockpit equipment, process and the driving of hardware board；In this reality
In applying example, the software kit run on interface computer 501 drives containing network communication, signal condition, Signal acquiring and processing, signal
And real-time process management etc. module.
Avionics system simulator 6 is used to complete the avionics display ＆ control system emulation of aircraft；In the present embodiment, avionics simulation computer
601 are realized by the way of " industrial computer+reflective memory card ", are responsible for completing the Models computed of aircraft avionics system, shown in real time
With control, it has bidirectional information transitive relation between main flight simulation computer 101；The basis of avionics display panel control 602
Aeroplane cloth office is separately mounted to relevant position in aircraft nacelle 701.Avionics simulation software is run on avionics simulation computer 601,
The avionics simulation software includes the modules such as control pipe is managed, instrument shows, navigates, communicating.
In the present embodiment, avionics display ＆ control system simulation package shows, controls, navigates, communicates containing the avionics related to flight
And alarm function simulation.
Analog capsule cabin 7 is used to complete the passenger cabin operating environment real-time simulation of aircraft；In the present embodiment, nacelle 701 is adopted
Semi-monocoque thin-wall construction, head profile and windscreen profile are designed processing according to aircraft configuration；Nacelle 701 and passenger cabin platform
Closely it is reliably connected together by transition piece between 702；Cockpit equipment 703 and passenger cabin are electrically and the basis of lighting unit 704
Aeroplane cloth office is separately mounted to relevant position in aircraft nacelle 701.
In the present embodiment, passenger cabin operating environment real-time simulation includes aircraft cockpit nacelle, seat, front panel, front
The true simulation of control panel, center console, left and right console and cockpit equipment.
Vision simulation unit 8 is used to complete the simulation of scene out of my cabin of aircraft；In the present embodiment, vision simulation computer
801 adopt professional graphic work station, and for generating corresponding scenic picture in real time, it is between main flight simulation computer 101
There is information transfering relation；Projector 802 and display ball curtain 803 collectively constitute visual display unit, for scenic picture
Show in real time, be separately mounted on passenger cabin platform 702.
In the present embodiment, visual effect of the scene simulation out of my cabin comprising different flight state under various meteorological conditions and
The real-time simulation of various natural scenes and its relative motion dynamic effect.
Speech simulation unit 9 is used for various environment sound equipments emulation that control completes flight course；In the present embodiment, sound
Simulation computer 901 realizes that it is deposited between main flight simulation computer 101 by the way of " industrial computer+reflective memory card "
In information transfering relation.
In the present embodiment, various environment sound equipment simulation packages containing the engine operating sound sent in aircraft flight,
Thunder, the patter of rain that undercarriage control sound, alarm sound and external environment send.
Environment completes power supply management, air conditioner ventilation and smoke detection with alarm emulation with supporter 10 for control；
In the present embodiment, power management unit 1001 is responsible for providing AC and DC voltage-stabilized power supply；Air-conditioner ventilation unit 1002 is responsible for completing
Temperature monitoring and Ventilation Control in nacelle 701；Smoke detection Alarm Unit 1003 is responsible for completing the smog prison in nacelle 701
Survey and automatic alarm.
The real-time network unit 11 is used for real time data between each modular unit that control is completed in aircraft flight
Exchange with communication.Real-time network switch 1101 is all connected with main flight simulation computer 101, control with reflective memory card 1102
Tubulation reason computer 202, record analysis shows computer 203, manipulation/motion simulation computer 402, interface computer 501, boat
Electric simulation computer 601, vision simulation computer 801 and sound simulation computer 901.
It is last it is to be noted that：Above example is only illustrating the technical solution of the utility model, rather than it is limited
System.Although being described in detail to the utility model with reference to the foregoing embodiments, one of ordinary skill in the art should manage
Solution：It still can modify to the technical scheme described in foregoing embodiments, or which part technical characteristic is entered
Row equivalent；And these modifications or replacement, do not make each embodiment of essence disengaging the utility model of appropriate technical solution
The spirit and scope of technical scheme.
Claims (9)
1. a kind of aircraft flight simulation experimental rig, it is characterised in that：Comprising main flight simulator (1), comprehensive control management device
(2) load cell (3), kinematic system unit (4), are manipulated, interface unit (5), avionics system simulator (6), analog capsule cabin (7), is regarded
Scape simulation unit (8), speech simulation unit (9), environment and supporter (10), real-time network unit (11)；
The main flight simulator (1) completes the flight course emulation of aircraft for control；
The comprehensive control management device (2) completes the task scheduling of aircraft for control and management and the analysis of flying quality are commented
Estimate；
The manipulation load device that load cell (3) is manipulated for controlling to complete aircraft is emulated；
The kinematic system unit (4) feels emulation for the instantaneous overload that control completes aircraft；
The interface unit (5) for complete aircraft cockpit equipment signals collecting, process and hardware board driving；
The avionics system simulator (6) emulates for the avionics display ＆ control system for completing aircraft；
The analog capsule cabin (7) is for completing the passenger cabin operating environment real-time simulation of aircraft；
The vision simulation unit (8) is simulated for the scene out of my cabin for completing aircraft；
The speech simulation unit (9) completes various environment sound equipments emulation of flight course for control；
It is imitative with alarm that the environment completes power supply management, air conditioner ventilation and smoke detection with supporter (10) for control
Very；
The real-time network unit (11) completes real time data between each modular unit in aircraft flight for control
Exchange and communication.
2. aircraft flight simulation experimental rig as claimed in claim 1, it is characterised in that：The flight course simulation package is containing winged
The flight simulation of flight simulation and flight envelope border of the machine within flight envelope, and can be to the event of appearance in flight course
Barrier carries out the simulation of quantitative or qualitative simulation.
3. aircraft flight simulation experimental rig as claimed in claim 1, it is characterised in that：The task scheduling with management and
The analysis and evaluation of flying quality includes test, the setting of topic of taking a flight test；Flight environment of vehicle, airport condition Initialize installation；Aircraft event
The setting of barrier and special circumstances；Flight course is monitored；The record of flying quality, playback and analysis and evaluation.
4. aircraft flight simulation experimental rig as claimed in claim 1, it is characterised in that：The manipulation load device simulation package
Containing the static and dynamic c haracteristics simulation under different flying conditions with different operating pattern lower-pilot systems, provide driving to pilot
Manipulation force feeling during actual airplane.
5. aircraft flight simulation experimental rig as claimed in claim 1, it is characterised in that：The instantaneous overload feels simulation package
Six-freedom motion simulated behavior containing aircraft longitudinal direction, lifting, lateral, pitching, roll and course, and to taking off,
Land is contacted to earth, stall is buffeted the dynamic of process and is simulated.
6. aircraft flight simulation experimental rig as claimed in claim 1, it is characterised in that：The avionics display ＆ control system simulation package
Show, control, navigating, communicating containing the avionics related to flight and alarm function simulation.
7. aircraft flight simulation experimental rig as claimed in claim 1, it is characterised in that：The passenger cabin operating environment is imitated in real time
Really include aircraft cockpit nacelle, seat, front panel, front control panel, center console, left and right console and cockpit equipment
True simulation.
8. aircraft flight simulation experimental rig as claimed in claim 1, it is characterised in that：The simulation of scene out of my cabin is comprising more
The visual effect and various natural scenes of different flight state and its relative motion dynamic effect is real-time under kind of meteorological condition
Emulation.
9. aircraft flight simulation experimental rig as claimed in claim 1, it is characterised in that：Various environment sound equipment simulation packages
Send containing engine operating sound, undercarriage control sound, alarm sound and the external environment sent in aircraft flight
Thunder, the patter of rain.
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| CN201620515037.2U CN206115770U (en) | 2016-05-31 | 2016-05-31 | Aircraft flight analogue test device |
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| CN201620515037.2U CN206115770U (en) | 2016-05-31 | 2016-05-31 | Aircraft flight analogue test device |
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| CN107132773A (en) * | 2017-07-06 | 2017-09-05 | 中国航空工业集团公司西安飞机设计研究所 | A kind of airborne central maintenance application software checking system and method |
| CN107464471A (en) * | 2017-08-09 | 2017-12-12 | 上海工程技术大学 | A kind of display system and control method for flight simulator |
| CN107748492A (en) * | 2017-09-08 | 2018-03-02 | 中国飞行试验研究院 | Aircraft PIO takes a flight test instruction trace device and method of work |
| CN107886800A (en) * | 2017-11-28 | 2018-04-06 | 浙江中航通飞研究院有限公司 | A kind of aircraft cockpit avionics simulation system of people in the loop |
| CN107945615A (en) * | 2017-12-08 | 2018-04-20 | 中国航空工业集团公司成都飞机设计研究所 | A kind of method of real-time analog simulation engine |
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| CN110096006A (en) * | 2019-04-19 | 2019-08-06 | 常宁(常州)数据产业研究院有限公司 | A kind of automated driving system test device |
| CN111047946A (en) * | 2020-01-14 | 2020-04-21 | 中仿智能科技（上海）股份有限公司 | Full-function flight simulator |
| CN112783004A (en) * | 2020-12-29 | 2021-05-11 | 中国航空工业集团公司西安飞机设计研究所 | Redundancy simulation system for flight control computer of high-level simulator |
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| CN107464471B (en) * | 2017-08-09 | 2019-09-10 | 上海工程技术大学 | A kind of display system and control method for flight simulator |
| CN107464471A (en) * | 2017-08-09 | 2017-12-12 | 上海工程技术大学 | A kind of display system and control method for flight simulator |
| CN109147467B (en) * | 2017-08-22 | 2021-05-04 | 南京乐飞航空技术有限公司 | Helicopter control load system based on actual-mounted control lever system and simulation implementation method |
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| CN107748492A (en) * | 2017-09-08 | 2018-03-02 | 中国飞行试验研究院 | Aircraft PIO takes a flight test instruction trace device and method of work |
| CN107886800A (en) * | 2017-11-28 | 2018-04-06 | 浙江中航通飞研究院有限公司 | A kind of aircraft cockpit avionics simulation system of people in the loop |
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| CN110096006A (en) * | 2019-04-19 | 2019-08-06 | 常宁(常州)数据产业研究院有限公司 | A kind of automated driving system test device |
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| CN111047946A (en) * | 2020-01-14 | 2020-04-21 | 中仿智能科技（上海）股份有限公司 | Full-function flight simulator |
| CN112783004A (en) * | 2020-12-29 | 2021-05-11 | 中国航空工业集团公司西安飞机设计研究所 | Redundancy simulation system for flight control computer of high-level simulator |
| CN112783004B (en) * | 2020-12-29 | 2023-01-13 | 中国航空工业集团公司西安飞机设计研究所 | Redundancy simulation system for flight control computer of high-level simulator |
| CN112965398B (en) * | 2021-02-18 | 2022-10-11 | 江西洪都航空工业集团有限责任公司 | Electromechanical integrated management system test verification platform with load power simulation function |
| CN112965398A (en) * | 2021-02-18 | 2021-06-15 | 江西洪都航空工业集团有限责任公司 | Electromechanical integrated management system test verification platform with load power simulation function |
| CN113096484A (en) * | 2021-04-15 | 2021-07-09 | 中国人民解放军空军军医大学 | Design method of space directional obstacle flight simulation equipment |
| CN113377027A (en) * | 2021-05-26 | 2021-09-10 | 中国航空工业集团公司沈阳飞机设计研究所 | Aircraft propulsion system test system |
| CN113342068A (en) * | 2021-06-04 | 2021-09-03 | 中国民航大学 | Smoke flow control experiment system based on online machine learning |
| CN113342068B (en) * | 2021-06-04 | 2022-08-05 | 中国民航大学 | Smoke flow control experiment system based on online machine learning |
| CN114019939A (en) * | 2021-11-03 | 2022-02-08 | 商飞软件有限公司 | Civil aircraft cockpit distributed simulation system |
| CN114973847A (en) * | 2022-05-23 | 2022-08-30 | 安胜（天津）飞行模拟系统有限公司 | Method for simulating regional weather scene on flight simulator |
| CN114973847B (en) * | 2022-05-23 | 2024-04-12 | 安胜（天津）飞行模拟系统有限公司 | Method for simulating regional weather scene on flight simulator |
| CN115811373A (en) * | 2023-02-16 | 2023-03-17 | 星航互联(北京)科技有限公司 | Communication verification system and method for aircraft front cabin and storage medium |
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