CN107038309A - A kind of aircraft engine simulation teching system and method - Google Patents

A kind of aircraft engine simulation teching system and method Download PDF

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CN107038309A
CN107038309A CN201710259979.8A CN201710259979A CN107038309A CN 107038309 A CN107038309 A CN 107038309A CN 201710259979 A CN201710259979 A CN 201710259979A CN 107038309 A CN107038309 A CN 107038309A
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simulation
data
subsystem
engine
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CN107038309B (en
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董琦立
戴黎明
陶霁
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HANGKE TECHNOLOGY DEVELOPMENT Co.,Ltd.
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Chengdu Albert Technology Co Ltd
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    • 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
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    • G06T17/00Three dimensional [3D] modelling, e.g. data description of 3D objects

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Abstract

The invention discloses a kind of aircraft engine simulation teching system and method, described system includes data simulation subsystem and threedimensional model creates subsystem;Data simulation subsystem is used for the data simulation model and correlation properties simulation model for building aircraft engine, and receive the engine control data of outside, carry out parsing and obtain control command, the control command that the data simulation model of aircraft engine, correlation properties simulation model and parsing are obtained is supplied to threedimensional model to create subsystem;Threedimensional model create subsystem be used for according to from data simulation subsystem information loading engines three-dimensional model, control engines three-dimensional model sport, and receive outside render display control data, to engines three-dimensional model carry out special efficacy render and show.The present invention by way of threedimensional model builds and is combined, can intuitively show the running status of aircraft engine data simulation in teaching process, be conducive to improving the teaching environment of aircraft engine, improve efficiency of teaching.

Description

A kind of aircraft engine simulation teching system and method
Technical field
The present invention relates to a kind of aircraft engine simulation teching system and method.
Background technology
With the reach of science and the continuous progress of society, air equipment(Such as aircraft)Played in military and civilian More and more important effect, engine is building block important on aircraft, power needed for being provided for the flight for aircraft, The performance, reliability and economy of aircraft can be directly affected;In the teaching of all kinds of aeronautical engineering institutes, aircraft engine Occupy highly important status in theory teaching.
But it is due to the particularity of the complexity of aircraft engine in itself and its working environment, causes engine professional entity Teaching is carried out very difficult;Current domestic all types of aviation universities and colleges are due to the limitation of teaching equipment, in engine teaching work In work by the way of traditional and pattern carry out engine theory teaching;By student after engine specialized courses to engine Understanding also in the theory stage being related on textbook;Faculty can not directly show the running status of aircraft engine, learn It is raw also can not directly observation airplane engine running situation;It is unfavorable for integrading theory with practice realizing aircraft engine The teaching of machine relevant knowledge;Therefore domestic air mail engine art causes the sector due to the delayed of engine teaching at present Development substantially falls behind foreign countries, the need for domestic related teaching method is not enough to the Engine Industry development of support Domestic Aircraft, because This, which changes current teaching environment, becomes particularly important.
The content of the invention
It is an object of the invention to overcome the deficiencies of the prior art and provide a kind of aircraft engine simulation teching system and side Method, data simulation model by way of threedimensional model is created and is combined, can intuitively show aircraft in teaching process The running status of engine, is conducive to improving the teaching environment of aircraft engine, improves efficiency of teaching.
The purpose of the present invention is achieved through the following technical solutions:A kind of aircraft engine simulation teching system, bag Include:
Data simulation subsystem, for building the data simulation model and correlation properties simulation model of aircraft engine, and is received Outside engine control data, carries out parsing and obtains control command, then the data simulation model of aircraft engine, correlation is special Property simulation model and the obtained control command of parsing be supplied to threedimensional model to create subsystem;
Wherein, correlation properties simulation model includes fuel data simulation model, fuel oil control simulation model, air data emulation mould Type, source of the gas simulation model, exhaust simulation model, ignition system data model and engine starting system are from inactive state at a high speed The continuous exercise data model of motion;Specifically, described data simulation subsystem includes:Engine emulation module, for structure The data simulation model of aircraft engine is built, to set up the mathematical relationship of each skeletal structure of engine, aircraft engine is reacted Parameter and physical characteristic, and be supplied to threedimensional model create subsystem;Fuel oil emulation module, for building aircraft engine Fuel data simulation model and fuel oil control simulation model, and it is supplied to threedimensional model to create subsystem;Described fuel data Simulation model includes physical model, temperature model and the fluid data model fuel oil in itself;Described fuel oil control simulation model Include the physical model and motion model of aircraft engine intermediate fuel oil control module;Air fluid emulation module, it is winged for building Air data simulation model, source of the gas simulation model and the exhaust simulation model of machine engine, and it is supplied to threedimensional model to create son System;Described air data simulation model includes air characteristics model, air fluid data model and air themperature model;Hair Motivation start emulation module, for build engine igniting system data model and engine starting system from inactive state to The continuous exercise data model of high-speed motion, and it is supplied to threedimensional model to create subsystem;Engine control module, receives outside Engine control data, carry out parsing obtain control command, and by control command be supplied to threedimensional model create subsystem.
Threedimensional model creates subsystem, for loading engines three-dimensional mould according to the information from data simulation subsystem Type, controls engines three-dimensional model sport, and receive outside render display control data, engines three-dimensional model is carried out special Effect is rendered and shown.Specifically, described threedimensional model creates subsystem and included:Threedimensional model load-on module, for according to next Loaded from the information of engine emulation module, fuel oil emulation module, air fluid emulation module and engine start emulation module The threedimensional model of aircraft engine;Threedimensional model motion module, for control command of the basis from engine control module, plus The animation of each skeletal structure of load engines three-dimensional model simultaneously controls engines three-dimensional model sport;Threedimensional model rendering module, Special efficacy to engines three-dimensional model is rendered, and the threedimensional model special efficacy rendered includes temperature and changes special efficacy and device damage spy Effect;Threedimensional model display module, for being shown to engines three-dimensional model real-time animation, motion conditions and model special efficacy, The display mode of threedimensional model display module includes overall display, perspective display, part display and dynamic resolution and shown;Comprehensive control Molding block, outside for receiving renders display control data, to the render effects and threedimensional model of threedimensional model rendering module The display mode of display module is controlled.
Preferably, described aircraft engine simulation teching system also includes outside device for controlling engine, for Engine control data is provided in data simulation subsystem.The device for controlling engine is the air equipment of specialty, such as throttle platform Deng.
Preferably, described aircraft engine simulation teching system also includes outside threedimensional model control device, is used for Subsystem offer, which is created, to threedimensional model renders display control data.The threedimensional model control device includes PC computers or mobile hand Terminal is held, mainly using mobile handheld terminal, including mobile phone or ipad.
A kind of teaching method of described aircraft engine simulation teching system, comprises the following steps:
S1. data simulation subsystem builds the data simulation model and correlation properties simulation model of aircraft engine, and is supplied to Threedimensional model creates subsystem;
S2. threedimensional model creates subsystem and loads engines three-dimensional model according to the information from data simulation subsystem;
S3. the engine control data outside the reception of data simulation subsystem, carries out parsing acquisition control command and is supplied to three-dimensional Model creation subsystem, creates subsystem according to the control command received, loading engines three-dimensional model is each by threedimensional model The animation of individual skeletal structure simultaneously controls engines three-dimensional model sport;
S4. threedimensional model creates and renders display control data outside subsystem reception;
S5. threedimensional model creates subsystem and the special efficacy of engines three-dimensional model is rendered according to the control data received;
S6. threedimensional model creates subsystem according to the control data received to engines three-dimensional model real-time animation, motion feelings Condition and model special efficacy are shown.
Wherein, described step S1 includes following sub-step:
Data simulation subsystem builds the data simulation model of aircraft engine, sets up the mathematics pass of each skeletal structure of engine System, reacts the parameter and physical characteristic of aircraft engine, and is supplied to threedimensional model to create subsystem;
Data simulation subsystem builds the fuel data simulation model and fuel oil control simulation model of aircraft engine, and is supplied to Threedimensional model creates subsystem;Described fuel data simulation model includes physical model, temperature model and the stream fuel oil in itself Volume data model;Described fuel oil control simulation model includes physical model and the motion of aircraft engine intermediate fuel oil control module Model;
Data simulation subsystem builds the air data simulation model, source of the gas simulation model and exhaust emulation mould of aircraft engine Type, and it is supplied to threedimensional model to create subsystem;Described air data simulation model includes air characteristics model, air fluid Data model and air themperature model;
Data simulation subsystem builds engine igniting system data model and engine starting system from inactive state to height The continuous exercise data model of speed motion, and it is supplied to threedimensional model to create subsystem.
The special efficacy of engines three-dimensional model described in step S5 includes temperature and changes special efficacy and device damage special efficacy;Step S6 Described in the display mode of engines three-dimensional model include overall display, perspective display, part display and dynamic resolution and show.
The beneficial effects of the invention are as follows:(1)Data simulation model by way of threedimensional model is created and is combined, in religion The running status of aircraft engine can be intuitively shown during, is conducive to improving the teaching environment of aircraft engine, carries High efficiency of teaching.
(2)Engine control data can be provided into data simulation subsystem by outside device for controlling engine, Received, parsed to obtain control command by engine control module again, be supplied to threedimensional model to create subsystem control command, Engines three-dimensional model sport is controlled, the operability during simulation teching is improved.
(3)It can create subsystem offer by outside threedimensional model control device to threedimensional model and render display control Data processed, then by comprehensive control module receive control data, the render effects and threedimensional model of threedimensional model rendering module are shown Show that the display mode of module is controlled, improve the flexibility for rendering, showing during simulation teching.
Brief description of the drawings
Fig. 1 is system principle diagram of the invention;
Fig. 2 is flow chart of the method for the present invention.
Embodiment
Technical scheme is described in further detail below in conjunction with the accompanying drawings, but protection scope of the present invention is not limited to It is as described below.
As shown in figure 1, a kind of aircraft engine simulation teching system, including:
Data simulation subsystem, for building the data simulation model and correlation properties simulation model of aircraft engine, and is received Outside engine control data, carries out parsing and obtains control command, then the data simulation model of aircraft engine, correlation is special Property simulation model and the obtained control command of parsing be supplied to threedimensional model to create subsystem;
In embodiments herein, correlation properties simulation model include fuel data simulation model, fuel oil control simulation model, Air data simulation model, source of the gas simulation model, exhaust simulation model, ignition system data model and engine starting system from Continuous exercise data model of the inactive state to high-speed motion;Accordingly, described data simulation subsystem includes:Engine is imitated True module, the data simulation model for building aircraft engine, to set up the mathematical relationship of each skeletal structure of engine, instead The parameter and physical characteristic of aircraft engine are answered, and is supplied to threedimensional model to create subsystem;Fuel oil emulation module, for building Fuel data simulation model and fuel oil the control simulation model of aircraft engine, and it is supplied to threedimensional model to create subsystem;Institute The fuel data simulation model stated includes physical model, temperature model and the fluid data model fuel oil in itself;Described fuel oil Control simulation model includes the physical model and motion model of aircraft engine intermediate fuel oil control module;Air fluid emulation mould Block, for building the air data simulation model, source of the gas simulation model and exhaust simulation model of aircraft engine, and is supplied to three Dimension module creates subsystem;Described air data simulation model includes air characteristics model, air fluid data model and sky Gas temperature model;Engine start emulation module, for building engine igniting system data model and engine start system The continuous exercise data model united from inactive state to high-speed motion, and it is supplied to threedimensional model to create subsystem;Engine control Engine control data outside molding block, reception, carries out parsing and obtains control command, and control command is supplied into three-dimensional mould Type creates subsystem.
Threedimensional model creates subsystem, for loading engines three-dimensional mould according to the information from data simulation subsystem Type, controls engines three-dimensional model sport, and receive outside render display control data, engines three-dimensional model is carried out special Effect is rendered and shown.Specifically, described threedimensional model creates subsystem and included:Threedimensional model load-on module, for according to next Loaded from the information of engine emulation module, fuel oil emulation module, air fluid emulation module and engine start emulation module The threedimensional model of aircraft engine;Threedimensional model motion module, for control command of the basis from engine control module, plus The animation of each skeletal structure of load engines three-dimensional model simultaneously controls engines three-dimensional model sport;Threedimensional model rendering module, Special efficacy to engines three-dimensional model is rendered, and the threedimensional model special efficacy rendered includes temperature and changes special efficacy and device damage spy Effect;Threedimensional model display module, for being shown to engines three-dimensional model real-time animation, motion conditions and model special efficacy, The display mode of threedimensional model display module includes overall display, perspective display, part display and dynamic resolution and shown;Comprehensive control Molding block, outside for receiving renders display control data, to the render effects and threedimensional model of threedimensional model rendering module The display mode of display module is controlled.
The application data simulation model with threedimensional model create be combined by way of, can be directly perceived in teaching process Ground shows the running status of aircraft engine, is conducive to improving the teaching environment of aircraft engine, improves efficiency of teaching.
In embodiments herein, described aircraft engine simulation teching system also includes outside engine control Equipment, for providing engine control data into data simulation subsystem.The device for controlling engine sets for the aviation of specialty It is standby, such as throttle platform;In teaching process, faculty can pass through device for controlling engine(Throttle platform etc.)To engine Threedimensional model is controlled, and is received by the engine control module in data simulation subsystem, is parsed to obtain control command, will Control command is supplied to threedimensional model to create subsystem, controls engines three-dimensional model sport, and show mould by threedimensional model Block shows student, improves the operability during simulation teching.
In embodiments herein, described aircraft engine simulation teching system also includes outside threedimensional model control Control equipment, display control data are rendered for creating subsystem offer to threedimensional model.The threedimensional model control device includes PC Computer or mobile handheld terminal, mainly using mobile handheld terminal, including mobile phone or ipad, in teaching process, faculty Threedimensional model control device can be passed through(PC computers, mobile phone, ipad etc.)Special efficacy to engines three-dimensional model is rendered(Temperature changes Become special efficacy and device damage special efficacy)It is controlled, can also be to the display mode of threedimensional model display module(It is overall to show, thoroughly Shown depending on display, part display and dynamic resolution)Be controlled, improve render during simulation teching, show it is flexible Property.
As shown in Fig. 2 a kind of teaching method of described aircraft engine simulation teching system, comprises the following steps:
S1. data simulation subsystem builds the data simulation model and correlation properties simulation model of aircraft engine, and is supplied to Threedimensional model creates subsystem;In embodiments herein, described step S1 includes following sub-step:Data simulation subsystem System builds the data simulation model of aircraft engine, sets up the mathematical relationship of each skeletal structure of engine, reacts aircraft engine The parameter and physical characteristic of machine, and it is supplied to threedimensional model to create subsystem;Data simulation subsystem builds aircraft engine Fuel data simulation model and fuel oil control simulation model, and it is supplied to threedimensional model to create subsystem;Described fuel data Simulation model includes physical model, temperature model and the fluid data model fuel oil in itself;Described fuel oil control simulation model Include the physical model and motion model of aircraft engine intermediate fuel oil control module;Data simulation subsystem builds aircraft engine Air data simulation model, source of the gas simulation model and exhaust simulation model, and be supplied to threedimensional model create subsystem;It is described Air data simulation model include air characteristics model, air fluid data model and air themperature model;Data simulation The continuous fortune of system constructing engine igniting system data model and engine starting system from inactive state to high-speed motion Dynamic data model, and it is supplied to threedimensional model to create subsystem;
S2. threedimensional model creates subsystem and loads engines three-dimensional model according to the information from data simulation subsystem;
S3. the engine control data outside the reception of data simulation subsystem, carries out parsing acquisition control command and is supplied to three-dimensional Model creation subsystem, creates subsystem according to the control command received, loading engines three-dimensional model is each by threedimensional model The animation of individual skeletal structure simultaneously controls engines three-dimensional model sport;
S4. threedimensional model creates and renders display control data outside subsystem reception;
S5. threedimensional model creates subsystem and the special efficacy of engines three-dimensional model is rendered according to the control data received; Wherein, the special efficacy of engines three-dimensional model includes temperature change special efficacy and device damage special efficacy.
S6. threedimensional model creates subsystem according to the control data received to engines three-dimensional model real-time animation, fortune Emotionally condition and model special efficacy are shown;In the application in embodiment, the display mode of engines three-dimensional model includes overall It has been shown that, perspective display, part display and dynamic resolution are shown.

Claims (10)

1. a kind of aircraft engine simulation teching system, it is characterised in that:Including:
Data simulation subsystem, for building the data simulation model and correlation properties simulation model of aircraft engine, and is received Outside engine control data, carries out parsing and obtains control command, then the data simulation model of aircraft engine, correlation is special Property simulation model and the obtained control command of parsing be supplied to threedimensional model to create subsystem;
Threedimensional model creates subsystem, for loading engines three-dimensional model, control according to the information from data simulation subsystem Engines three-dimensional model sport processed, and receive outside render display control data, to engines three-dimensional model carry out special efficacy wash with watercolours Dye and display.
2. a kind of aircraft engine simulation teching system according to claim 1, it is characterised in that:Described data simulation Subsystem includes:
Engine emulation module, the data simulation model for building aircraft engine, to set up engine each skeletal structure Mathematical relationship, react aircraft engine parameter and physical characteristic, and be supplied to threedimensional model create subsystem;
Fuel oil emulation module, for building the fuel data simulation model and fuel oil control simulation model of aircraft engine, and is carried Supply threedimensional model and create subsystem;Described fuel data simulation model includes physical model, the temperature model fuel oil in itself With fluid data model;Described fuel oil control simulation model include aircraft engine intermediate fuel oil control module physical model and Motion model;
Air fluid emulation module, air data simulation model, source of the gas simulation model and exhaust for building aircraft engine Simulation model, and it is supplied to threedimensional model to create subsystem;Described air data simulation model includes air characteristics model, sky Air-flow volume data model and air themperature model;
Engine start emulation module, for building engine igniting system data model and engine starting system from static State to high-speed motion continuous exercise data model, and be supplied to threedimensional model create subsystem;
Engine control module, receives outside engine control data, carries out parsing acquisition control command, and by control command It is supplied to threedimensional model to create subsystem.
3. a kind of aircraft engine simulation teching system according to claim 1, it is characterised in that:Described threedimensional model Creating subsystem includes:
Threedimensional model load-on module, for according to from engine emulation module, fuel oil emulation module, air fluid emulation module The threedimensional model of aircraft engine is loaded with the information of engine start emulation module;
Threedimensional model motion module, for according to the control command from engine control module, loading engines three-dimensional model The animation of each skeletal structure simultaneously controls engines three-dimensional model sport;
Threedimensional model rendering module, the special efficacy to engines three-dimensional model is rendered, and the threedimensional model special efficacy rendered includes temperature Degree changes special efficacy and device damage special efficacy;
Threedimensional model display module, for being shown to engines three-dimensional model real-time animation, motion conditions and model special efficacy, The display mode of threedimensional model display module includes overall display, perspective display, part display and dynamic resolution and shown;
Comprehensive control module, outside for receiving renders display control data, to the render effects of threedimensional model rendering module It is controlled with the display mode of threedimensional model display module.
4. a kind of aircraft engine simulation teching system according to claim 1, it is characterised in that:Described aircraft engine Machine simulation teching system also includes outside device for controlling engine, for providing engine control into data simulation subsystem Data.
5. a kind of aircraft engine simulation teching system according to claim 4, it is characterised in that:Described engine control Control equipment is the air equipment of specialty, including throttle platform.
6. a kind of aircraft engine simulation teching system according to claim 1, it is characterised in that:Described aircraft engine Machine simulation teching system also includes outside threedimensional model control device, aobvious for being rendered to threedimensional model establishment subsystem offer Show control data.
7. a kind of aircraft engine simulation teching system according to claim 6, it is characterised in that:Described threedimensional model Control device includes PC computers or mobile handheld terminal, and the mobile handheld terminal includes mobile phone or ipad.
8. a kind of teaching method of aircraft engine simulation teching system as described in any one in claim 1 ~ 7, it is special Levy and be:Comprise the following steps:
S1. data simulation subsystem builds the data simulation model and correlation properties simulation model of aircraft engine, and is supplied to Threedimensional model creates subsystem;
S2. threedimensional model creates subsystem and loads engines three-dimensional model according to the information from data simulation subsystem;
S3. the engine control data outside the reception of data simulation subsystem, carries out parsing acquisition control command and is supplied to three-dimensional Model creation subsystem, creates subsystem according to the control command received, loading engines three-dimensional model is each by threedimensional model The animation of individual skeletal structure simultaneously controls engines three-dimensional model sport;
S4. threedimensional model creates and renders display control data outside subsystem reception;
S5. threedimensional model creates subsystem and the special efficacy of engines three-dimensional model is rendered according to the control data received;
S6. threedimensional model creates subsystem according to the control data received to engines three-dimensional model real-time animation, motion feelings Condition and model special efficacy are shown.
9. a kind of teaching method of aircraft engine simulation teching system according to claim 8, it is characterised in that:It is described Step S1 include following sub-step:
Data simulation subsystem builds the data simulation model of aircraft engine, sets up the mathematics pass of each skeletal structure of engine System, reacts the parameter and physical characteristic of aircraft engine, and is supplied to threedimensional model to create subsystem;
Data simulation subsystem builds the fuel data simulation model and fuel oil control simulation model of aircraft engine, and is supplied to Threedimensional model creates subsystem;Described fuel data simulation model includes physical model, temperature model and the stream fuel oil in itself Volume data model;Described fuel oil control simulation model includes physical model and the motion of aircraft engine intermediate fuel oil control module Model;
Data simulation subsystem builds the air data simulation model, source of the gas simulation model and exhaust emulation mould of aircraft engine Type, and it is supplied to threedimensional model to create subsystem;Described air data simulation model includes air characteristics model, air fluid Data model and air themperature model;
Data simulation subsystem builds engine igniting system data model and engine starting system from inactive state to height The continuous exercise data model of speed motion, and it is supplied to threedimensional model to create subsystem.
10. a kind of teaching method of aircraft engine simulation teching system according to claim 8, it is characterised in that:Step The special efficacy of engines three-dimensional model described in rapid S5 includes temperature and changes special efficacy and device damage special efficacy;Start described in step S6 The display mode of machine threedimensional model includes overall display, perspective display, part display and dynamic resolution and shown.
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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107515587A (en) * 2017-08-30 2017-12-26 工业和信息化部电子第五研究所华东分所 System, method, apparatus, equipment and the storage medium of man-machine interactive operation emulation
CN110310523A (en) * 2019-05-28 2019-10-08 云南东方飞行培训有限公司 Teaching method, system electronic device and storage medium based on mixed reality

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6606612B1 (en) * 1998-08-13 2003-08-12 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Method for constructing composite response surfaces by combining neural networks with other interpolation or estimation techniques
CN101561351A (en) * 2009-06-04 2009-10-21 中国航空工业集团公司西安飞机设计研究所 Airplane engine dynamic simulation test bed
CN103456202A (en) * 2013-09-05 2013-12-18 上海蔚翼航空科技有限公司 Analogue simulation device based on plane test flight training and system thereof
CN105976672A (en) * 2016-07-18 2016-09-28 成都艾尔伯特科技有限责任公司 Multifunctional flight teaching platform
CN106407570A (en) * 2016-09-22 2017-02-15 南京航空航天大学 An airplane assembling process online simulating optimization system
CN206058608U (en) * 2016-06-29 2017-03-29 成都艾尔伯特科技有限责任公司 Flight simulation recreation experience equipment

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6606612B1 (en) * 1998-08-13 2003-08-12 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Method for constructing composite response surfaces by combining neural networks with other interpolation or estimation techniques
CN101561351A (en) * 2009-06-04 2009-10-21 中国航空工业集团公司西安飞机设计研究所 Airplane engine dynamic simulation test bed
CN103456202A (en) * 2013-09-05 2013-12-18 上海蔚翼航空科技有限公司 Analogue simulation device based on plane test flight training and system thereof
CN206058608U (en) * 2016-06-29 2017-03-29 成都艾尔伯特科技有限责任公司 Flight simulation recreation experience equipment
CN105976672A (en) * 2016-07-18 2016-09-28 成都艾尔伯特科技有限责任公司 Multifunctional flight teaching platform
CN106407570A (en) * 2016-09-22 2017-02-15 南京航空航天大学 An airplane assembling process online simulating optimization system

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
王坤,胡贤跃,葛雅静: "《空客A320航空发动机虚拟仿真教学平台开发》", 《实验技术与管理》 *

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107515587A (en) * 2017-08-30 2017-12-26 工业和信息化部电子第五研究所华东分所 System, method, apparatus, equipment and the storage medium of man-machine interactive operation emulation
CN107515587B (en) * 2017-08-30 2020-07-07 工业和信息化部电子第五研究所华东分所 System, method, device, equipment and storage medium for man-machine interaction operation simulation
CN110310523A (en) * 2019-05-28 2019-10-08 云南东方飞行培训有限公司 Teaching method, system electronic device and storage medium based on mixed reality

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