CN110046455A - A kind of Flight Vehicle Design platform, Flight Vehicle Design and software simulation system and method - Google Patents

A kind of Flight Vehicle Design platform, Flight Vehicle Design and software simulation system and method Download PDF

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Publication number
CN110046455A
CN110046455A CN201910340325.7A CN201910340325A CN110046455A CN 110046455 A CN110046455 A CN 110046455A CN 201910340325 A CN201910340325 A CN 201910340325A CN 110046455 A CN110046455 A CN 110046455A
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Prior art keywords
aircraft
flight
vehicle design
component
data
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CN201910340325.7A
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CN110046455B (en
Inventor
白杨
谢岩
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Zhuhai Dachuan Aviation Technology Co Ltd
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Zhuhai Dachuan Aviation Technology Co Ltd
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    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00Computer-aided design [CAD]
    • G06F30/10Geometric CAD
    • G06F30/15Vehicle, aircraft or watercraft design
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00Computer-aided design [CAD]
    • G06F30/20Design optimisation, verification or simulation
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F2111/00Details relating to CAD techniques
    • G06F2111/20Configuration CAD, e.g. designing by assembling or positioning modules selected from libraries of predesigned modules
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02PCLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P90/00Enabling technologies with a potential contribution to greenhouse gas [GHG] emissions mitigation
    • Y02P90/30Computing systems specially adapted for manufacturing

Abstract

The invention discloses a kind of Flight Vehicle Design platform, Flight Vehicle Design and software simulation system and methods, and the system comprises Flight Vehicle Design platform, aircraft simulation system and machine riding manipulation equipment;The Flight Vehicle Design platform for designing dummy vehicle, and saves the configuration data of dummy vehicle;The aircraft simulation system, data communication is carried out with the Flight Vehicle Design platform, for receiving the configuration data of the dummy vehicle of Flight Vehicle Design platform, and scene of taking a flight test is provided for dummy vehicle, in addition, the aircraft simulation system is also used to receive the control command of aircraft handling commanding apparatus, realizes and takes a flight test under the control of control command.System and method is driven an airplane by simulated flight device, does not have any security risk, but also can hold various athletic competitions, science communication initiative spirit, the propulsion of power-assisted aeronautical popular science education.

Description

A kind of Flight Vehicle Design platform, Flight Vehicle Design and software simulation system and method
Technical field
The present invention relates to Flight Vehicle Design and simulation technical fields, and in particular to a kind of Flight Vehicle Design platform, aircraft Design and software simulation system and method.
Background technique
With the development of aircraft industry, aircraft is known by ordinary people already, but for design and manufacture aircraft, also It is a very mysterious thing, the Flight Vehicle Design software being currently known contributes to professional actual aircraft design, and user is It is Specialty Design teacher of aircraft manufacturers, ordinary people is difficult arriving for contact, and the threshold for becoming Flight Vehicle Design teacher is also Very high, a aircraft is few then several years from researching and developing to taking a flight test, more then decades.Global aeronautical popular science education is all mostly Visit aircraft, visit airport, the simple flight management of study, paper folding aircraft etc., the innovation of student can not be excited to think completely Peacekeeping manipulative ability.
Summary of the invention
Based on the deficiencies of the prior art, it is imitative that the present invention provides a kind of Flight Vehicle Design platform, Flight Vehicle Design and softwares True system and method, by Flight Vehicle Design platform, user can create aircraft according to the idea of oneself on computers Model, by Flight Vehicle Design and software simulation system and method, user can be according to the flight of the dummy vehicle of creation Device data, import data in flight Simulation System, and user can drive dummy vehicle examination in flight Simulation System Fly the aircraft of oneself creation.
The technical solution of the present invention is as follows:
A kind of Flight Vehicle Design platform, it is characterised in that: including aircraft assembly database and the total entrucking of virtual aircraft Between, it include the data model information that attached the aircraft all parts of actual airplane performance, number in aircraft assembly database It include the airframe structure part of various shapes, the airplane main wing of plurality of specifications, tailplane, vertical end according to the component in library The component models such as the wing, various types of engines, motor, fuel tank, battery, a variety of undercarriages, aircraft cockpit, performance parameter is such as Mass per volume, offer lift coefficient, resistance coefficient etc..The virtual aircraft assembly shop is used for the aircraft that will be selected Data model assembling configuration.
Further, the virtual aircraft assembly shop includes aircraft component collision detection module, aircraft component Automatic aligning module, aircraft geometry and performance data computing module;
The aircraft component collision detection module is used to detect the distance and positional relationship of aircraft component, and Component is adsorbed in threshold range;
The aircraft component automatic aligning module, the angle for splicing the binding face adjust automatically of aircraft component And alignment;
The aircraft geometry and performance data computing module, for according to model in scene position and type, calculate The performance parameter of aircraft component.
It further, further include rendering module, each component selection rendering difference that the rendering module is used for as aircraft Color.
It further, further include data preview and inspection panel module, the data preview and inspection panel module are used for The configuration parameter of the dummy vehicle of assembly is shown, it is determined whether meet design requirement.
A kind of Flight Vehicle Design and software simulation system, it is characterised in that: including Flight Vehicle Design platform, aerial vehicle simulation System and machine riding manipulation equipment;
The Flight Vehicle Design platform for designing dummy vehicle, and saves the configuration data of dummy vehicle;
The aircraft simulation system carries out data communication with the Flight Vehicle Design platform, sets for receiving aircraft The configuration data of the dummy vehicle of platform is counted, and provides scene of taking a flight test for dummy vehicle, in addition, the aerial vehicle simulation system System is also used to receive the control command of aircraft handling commanding apparatus, realizes and takes a flight test under the control of control command.
Further, the Flight Vehicle Design platform includes aircraft assembly database and virtual aircraft assembly shop, It include the data model information that attached the aircraft all parts of actual airplane performance, the void in aircraft assembly database Quasi- aircraft assembly shop is used to set the aircraft data model group assembly of selection;
The virtual aircraft assembly shop includes aircraft component collision detection module, aircraft component automatic aligning mould Block, aircraft geometry and performance data computing module;
The aircraft component collision detection module is used to detect the distance and positional relationship of aircraft component, and Component is adsorbed in threshold range;The aircraft component automatic aligning module, for by the fitting of aircraft component The angle and alignment of face adjust automatically splicing;
The aircraft geometry and performance data computing module, for according to model in scene position and type, calculate The performance parameter of aircraft component.
A kind of Flight Vehicle Design and sofeware simulation method, which is characterized in that the described method includes:
Step 1, dummy vehicle is designed on Flight Vehicle Design platform, and saves the configuration data of dummy vehicle;
Step 2, the configuration data of dummy vehicle is transferred to aircraft simulation system, aircraft simulation system is to configuration Data are parsed, and under the control of aircraft riding manipulation instruction, are taken a flight test in the scene of taking a flight test that aircraft provides.
Further, the method for design dummy vehicle includes: on Flight Vehicle Design platform in step 1
Step 11, the database or data of dummy vehicle all parts are established in based on 3D game engine exploitation environment File;
Step 12, dummy vehicle is selected to be assembled in dummy vehicle database, in an assembling process, to flight Device component carries out collision detection and automatic aligning, realizes the absorption of dummy vehicle component, by model automatic aligning, realizes and flies The angle of row device model splicing adjusts;
Step 13, the dummy vehicle data that design is completed are saved, and transmit the data to aircraft simulation system.
Further, the binding face obtained in model automatic aligning using absorption algorithm in step 12, self-optimizing model Splicing angle.
Further, geometry and property during being assembled in step 12 to dummy vehicle also by calculating aircraft Energy data obtain the performance parameter of each component.
The invention has the benefit that
Flight Vehicle Design platform reduces aeronautical popular science object, aerophile, ordinary people etc. and contacts Flight Vehicle Design door Sill, allow ordinary people also can by design flight come deeper into understanding aviation, recognize aviation;Profound level is greatly reduced simultaneously Aeronautical popular science education cost, and the innovative thinking and creativity of user can be excited;And aircraft simulation system is combined, lead to Simulated flight device is crossed to drive an airplane, does not have any security risk, but also various athletic competitions, science communication can be held Initiative spirit, the propulsion of power-assisted aeronautical popular science education.
Detailed description of the invention
Fig. 1 is the architecture diagram of Flight Vehicle Design of the invention and software simulation system.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other Embodiment shall fall within the protection scope of the present invention.
The Flight Vehicle Design platform of a kind of Flight Vehicle Design platform, the present embodiment is based on a three-dimensional scenic editing machine, can To use 3D game engine to develop, scene effect can accomplish true to nature, beautiful.Including aircraft assembly database, virtual flight Device assembly shop and display module further include interface of taking a flight test, and include that attached actual airplane performance in aircraft assembly database Aircraft all parts data model information, and can be shown in the menu bar of the display module, and selected for dragging, institute Virtual aircraft assembly shop is stated for setting the aircraft data model group assembly of selection, and can be shown on the display module Show the effect of assembly.Aircraft assembly database provides whole component models required for aircraft assembling, including various shapes The airframe structure part, airplane main wing of plurality of specifications, tailplane, vertical tail, various types of engines, electronic The components such as machine, fuel tank, battery, a variety of undercarriages, aircraft cockpit, and have in the menu bar of the display panel of display module pair Option is answered, all components attached attribute of performance all in accordance with the standard of actual airplane, and such as mass per volume provides lift system Number, resistance coefficient etc..Component in aircraft assembly database can be used the design of the 3 d modeling softwares such as 3DMax, model it is big Small scale is consistent with actual aircraft, and performance data design can decompose average according to the performance data of several typical actual airplanes Value.The data of dummy vehicle in flight component database are stored in database or data file according to tree structure.
The virtual aircraft assembly shop includes aircraft component collision detection module, aircraft component automatic aligning mould Block, aircraft geometry and performance data computing module.
The aircraft component collision detection module is used to detect the distance and positional relationship of aircraft component, and Component is adsorbed in threshold range.
The aircraft component automatic aligning module, the angle for splicing the binding face adjust automatically of aircraft component And alignment.
The aircraft geometry and performance data computing module, for according to model in scene position and type, calculate With the performance parameter after adjustment aircraft component assembling.
User in menu bar the input equipments such as mouse-keyboard can be used drag, assembled, adjustment aircraft all parts, During assembled by aircraft component collision detection module, aircraft component automatic aligning module come automatic absorbing, alignment and Splicing;By aircraft geometry and performance can calculating aircraft the parameters such as size, center of gravity and weight, for example, the span of aircraft To calculate the distance between two tips of two wings of aircraft to obtain, the weight of aircraft is the sum of the weight of all components, center of gravity according to Distribution of weight ratio calculating etc. can check the matter of designed aircraft by data preview and inspection panel in assembling process Whether amount balance, liter resistance, power matching etc. meet design requirement.
Flight Vehicle Design platform further includes rendering module, and the rendering module is used to select rendering for each component of aircraft Different colors, rendering module have the rendering window that can carry out multiple color selection on the display panel of display module Mouthful, it chooses and clicks the rendered color of selection after component again and can render different colors to the different components of aircraft.
Flight Vehicle Design platform further includes data preview and inspection panel module, the data preview and inspection panel module Configuration parameter for the dummy vehicle to assembly is shown, it is determined whether meets design requirement.Data preview and inspection Panel shows a floating window on display module panel, and the parameter of display dummy vehicle configuration in floating window, parameter includes fuselage The specification of constitutional detail, the model of engine and each part and the performance index of engine etc..
Flight Vehicle Design platform further includes VR equipment calls module, and the VR equipment calls module is connect by calling with computer Mouth is connected with VR equipment, and the design and assembly of aircraft is made to realize three-dimensional fill under mouse drag assembly and visual VR facility environment Match and shows.
As shown in Figure 1, a kind of Flight Vehicle Design and software simulation system, including Flight Vehicle Design platform, aerial vehicle simulation System, aircraft handling commanding apparatus and network system;
The Flight Vehicle Design platform for designing dummy vehicle under three-dimensional visible environment, and saves aircraft mould The configuration data of type;The Flight Vehicle Design platform Flight Vehicle Design platform disclosed above using the present embodiment.
The aircraft simulation system carries out data communication by the network equipment and the Flight Vehicle Design platform, is used for The configuration data of the dummy vehicle of Flight Vehicle Design platform is received, and provides scene of taking a flight test, the present embodiment for dummy vehicle The two is communicated to connect using Ethernet, in addition, the aircraft simulation system is also used to receive aircraft handling commanding apparatus Control command is realized under the control of control command and is taken a flight test.User can control the liter of aircraft by flight control bar apparatus The control planes such as rudder, aileron, rudder are dropped, the thrust of engine can be controlled by throttle lever.
Aircraft simulation system can be used Simlink and build, and quickly, facilitate debugging, aircraft simulation system can also be used The analogue system of general common aircraft, general aircraft simulation system includes aerodynamics module and engine mould Block, aerodynamics module are calculated in real time according to aerodynamic parameter, to attitude of flight vehicle angle, acceleration and are shown by real time data Show that module is shown, the engine driving gear calculating aircraft that engine block is used to input according to aircraft handling commanding apparatus is real When thrust and fuel consumption, aircraft latitude and longitude coordinates are sent to realtime curve module and are displayed data, are regarded simultaneously Scape module obtains the flight attitude data of aircraft in real time, with aircraft cabin visual angle real-time display flying scene in the scene.
The aircraft simulation system of use further includes sound simulation module, and the sound simulation module is different according to aircraft State generates and plays different audios.
A kind of Flight Vehicle Design and sofeware simulation method, which comprises
Step 1, dummy vehicle is designed on Flight Vehicle Design platform, and saves the configuration data of dummy vehicle;
Step 2, the configuration data of dummy vehicle is transferred to aircraft simulation system, aircraft simulation system is to configuration Data are parsed, and under the control of aircraft riding manipulation instruction, are taken a flight test in the scene of taking a flight test that aircraft provides.
The method of design dummy vehicle includes: on Flight Vehicle Design platform in step 1
Step 11, the database or data of dummy vehicle all parts are established in based on 3D game engine exploitation environment File;
Step 12, dummy vehicle is selected to be assembled in dummy vehicle database, in an assembling process, to flight Device component carries out collision detection and automatic aligning, realizes the absorption of dummy vehicle component, by model automatic aligning, realizes and flies The angle of row device model splicing adjusts;
Step 13, the dummy vehicle data that design is completed are saved, and transmit the data to aircraft simulation system.
The binding face obtained in model automatic aligning using absorption algorithm in step 12, the splicing angle of self-optimizing model Degree.
It is also obtained by the geometry and performance data that calculate aircraft during being assembled in step 12 to dummy vehicle The performance parameter of each component out.The position according to model in scene and type are specifically included, the length of aircraft, the exhibition of wing are calculated Width, the chord length of wing, the weight of aircraft, position of centre of gravity, motor power position of centre of gravity, air force position of centre of gravity.
The present embodiment uses Flight Vehicle Design Platform Designing dummy vehicle, and saves the data of dummy vehicle, then will The basic data of the dummy vehicle of preservation is transferred to aircraft simulation system by network system, and aircraft simulation system is base Plinth data configuration generates the Math parameter of aircraft simulation system, and aircraft simulation system is in aircraft handling commanding apparatus Manipulation is lower to realize simulated flight, by experiencing simulated effect in what comes into a driver's module, experience of really taking a flight test to people.
Present invention reduces aeronautical popular science object, aerophile, ordinary peoples etc. to contact Flight Vehicle Design threshold, allows common People also can by design flight come deeper into understanding aviation, recognize aviation.Greatly reduce profound aeronautical popular science religion The cost educated, and the innovative thinking and creativity of user can be excited.It is driven an airplane, is not had any by simulated flight device Security risk;Meanwhile user can not only be transformed the aircraft of the design of oneself, and can also be by the aircraft of creation It can be shared by forms such as online network, storage mediums with other people;Various sports ratios can be held by using the present invention Match, science communication initiative spirit, the propulsion of power-assisted aeronautical popular science education.
It although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with A variety of variations, modification, replacement can be carried out to these embodiments without departing from the principles and spirit of the present invention by understanding And modification, the scope of the present invention is defined by the appended.

Claims (10)

1. a kind of Flight Vehicle Design platform, it is characterised in that: including aircraft assembly database and virtual aircraft assembly shop, It include the data model information that attached the aircraft all parts of actual airplane performance, the void in aircraft assembly database Quasi- aircraft assembly shop is used to set the aircraft data model group assembly of selection.
2. Flight Vehicle Design platform as described in claim 1, it is characterised in that: the virtual aircraft assembly shop includes flying Row device component collision detection module, aircraft component automatic aligning module, aircraft geometry and performance data computing module;
The aircraft component collision detection module is used to detect the distance and positional relationship of aircraft component, and in valve Component is adsorbed within the scope of value;
The aircraft component automatic aligning module, for by the angle of the binding face adjust automatically of aircraft component splicing and right Together;
The aircraft geometry and performance data computing module, for according to model in scene position and type, calculate flight The performance parameter of each component of device.
3. Flight Vehicle Design platform as described in claim 1, it is characterised in that: it further include rendering module, the rendering module Different colors is rendered for each component selection for aircraft.
4. Flight Vehicle Design platform as described in any one of claims 1-3, it is characterised in that: further include data preview and inspection Panel module, the data preview and inspection panel module be used to show the configuration parameter of the dummy vehicle of assembly, Determine whether to meet design requirement.
5. a kind of Flight Vehicle Design and software simulation system, it is characterised in that: including Flight Vehicle Design platform, aerial vehicle simulation system System and machine riding manipulation equipment;
The Flight Vehicle Design platform for designing dummy vehicle, and saves the configuration data of dummy vehicle;
The aircraft simulation system carries out data communication with the Flight Vehicle Design platform, flat for receiving Flight Vehicle Design The configuration data of the dummy vehicle of platform, and scene of taking a flight test is provided for dummy vehicle, in addition, the aircraft simulation system is also For receiving the control command of aircraft handling commanding apparatus, realizes and take a flight test under the control of control command.
6. Flight Vehicle Design as claimed in claim 5 and software simulation system, it is characterised in that: the Flight Vehicle Design platform It include that attached actual airplane in aircraft assembly database including aircraft assembly database and virtual aircraft assembly shop The data model information of the aircraft all parts of performance, the virtual aircraft assembly shop are used for the aircraft number that will be selected It is set according to model group assembly;
The virtual aircraft assembly shop include aircraft component collision detection module, aircraft component automatic aligning module, Aircraft geometry and performance data computing module;
The aircraft component collision detection module is used to detect the distance and positional relationship of aircraft component, and in valve Component is adsorbed within the scope of value;The aircraft component automatic aligning module, for by the binding face of aircraft component from The angle and alignment of dynamic adjustment splicing;
The aircraft geometry and performance data computing module, for according to model in scene position and type, calculate flight The performance parameter of device component.
7. a kind of Flight Vehicle Design and sofeware simulation method, which is characterized in that the described method includes:
Step 1, dummy vehicle is designed on Flight Vehicle Design platform, and saves the configuration data of dummy vehicle;
Step 2, the configuration data of dummy vehicle is transferred to aircraft simulation system, aircraft simulation system is to configuration data It is parsed, and under the control of aircraft riding manipulation instruction, is taken a flight test in the scene of taking a flight test that aircraft provides.
8. Flight Vehicle Design as claimed in claim 7 and sofeware simulation method, which is characterized in that set in step 1 in aircraft The method of design dummy vehicle includes: on meter platform
Step 11, the database or data text of dummy vehicle all parts are established in based on 3D game engine exploitation environment Part;
Step 12, dummy vehicle is selected to be assembled in dummy vehicle database, in an assembling process, to aircraft portion Part carries out collision detection and automatic aligning, realizes the absorption of dummy vehicle component, by model automatic aligning, realizes aircraft The angle of model splicing adjusts;
Step 13, the dummy vehicle data that design is completed are saved, and transmit the data to aircraft simulation system.
9. Flight Vehicle Design as claimed in claim 8 and sofeware simulation method, it is characterised in that: model is automatically right in step 12 The binding face obtained in neat using absorption algorithm, the splicing angle of self-optimizing model.
10. Flight Vehicle Design as claimed in claim 8 and sofeware simulation method, it is characterised in that: to aircraft in step 12 Model also calculates performance, the parameter of aircraft by the geometry and performance data that calculate aircraft during being assembled.
CN201910340325.7A 2019-04-25 2019-04-25 Aircraft design platform, aircraft design and software simulation system and method Active CN110046455B (en)

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112150886A (en) * 2020-09-22 2020-12-29 中国商用飞机有限责任公司 Method for evaluating validity of data package test flight data of flight simulator
CN114516427A (en) * 2022-02-08 2022-05-20 上海斯化露航空科技发展有限公司 Simulation system and method for design detection of airplane cabin door
CN114516427B (en) * 2022-02-08 2024-05-14 上海斯化露航空科技发展有限公司 Simulation system and method for aircraft cabin door design detection

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101398860A (en) * 2007-09-25 2009-04-01 北京航空航天大学 Cooperating design method of aircraft control system in different areas based on PDM//matlab
CN105488251A (en) * 2015-11-13 2016-04-13 中国人民解放军国防科学技术大学 Distributed aircraft simulation platform and implementation method thereof
CN106202669A (en) * 2016-06-30 2016-12-07 北京航空航天大学 A kind of intellectualized battle flight simulation device

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101398860A (en) * 2007-09-25 2009-04-01 北京航空航天大学 Cooperating design method of aircraft control system in different areas based on PDM//matlab
CN105488251A (en) * 2015-11-13 2016-04-13 中国人民解放军国防科学技术大学 Distributed aircraft simulation platform and implementation method thereof
CN106202669A (en) * 2016-06-30 2016-12-07 北京航空航天大学 A kind of intellectualized battle flight simulation device

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
张文苑: "飞行器动力学虚拟样机模型库的研究", 《计算机仿真》 *
胡庆军: "航天器协同设计平台总体框架设计", 《计算机工程与科学》 *

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112150886A (en) * 2020-09-22 2020-12-29 中国商用飞机有限责任公司 Method for evaluating validity of data package test flight data of flight simulator
CN114516427A (en) * 2022-02-08 2022-05-20 上海斯化露航空科技发展有限公司 Simulation system and method for design detection of airplane cabin door
CN114516427B (en) * 2022-02-08 2024-05-14 上海斯化露航空科技发展有限公司 Simulation system and method for aircraft cabin door design detection

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