CN109871565A - A kind of integrated electronic system simulator of general-purpose aircraft - Google Patents
A kind of integrated electronic system simulator of general-purpose aircraft Download PDFInfo
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- CN109871565A CN109871565A CN201811344716.8A CN201811344716A CN109871565A CN 109871565 A CN109871565 A CN 109871565A CN 201811344716 A CN201811344716 A CN 201811344716A CN 109871565 A CN109871565 A CN 109871565A
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- 235000008434 ginseng Nutrition 0.000 claims abstract description 3
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- 238000003786 synthesis reaction Methods 0.000 claims description 19
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- 238000013461 design Methods 0.000 abstract description 3
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- 238000013178 mathematical model Methods 0.000 description 2
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Abstract
The invention discloses a kind of integrated electronic system simulators of general-purpose aircraft, it is characterised in that: Simulation Control (101) completes the job control that ginseng, pattern switching are adjusted to model emulation (103), model dynamic exciting (104), the initialization of what comes into a driver's (105), starting, stopping, dynamic；Comprehensive aobvious control emulation (102) completes the display picture and logic of integrated display, is completed at the same time communication, navigation, the control panel emulation for indicating record system；Model emulation (103) is used to emulate the equipment or module of avionics and Mechatronic Systems；Model dynamic exciting (104) completes the dynamic exciting of model emulation (103).The dynamic digitalized simulation problems of Development of Universal aircraft integrated electronic system are enough solved using the present invention, the lead time can be greatly shortened, development cost is greatly lowered, while can support the design iteration more taken turns, raising newly grinds the maturity of product, to control developing risk well.
Description
Technical field
The present invention relates to general-purpose aircraft integrated electronic system technical fields, more particularly to the one of a kind of 23 general-purpose aircrafts
Body electronic system simulator.
Background technique
General-purpose aircraft had not only included 25 non-civil aviation passenger transport aircrafts, but also further included light-duty fortune including 23 all aircrafts
Dynamic class aircraft and the homemade test class aircraft of airhog.Wherein 23 general-purpose aircrafts is all logical for several amount and type
With the important member of aircraft family, type is general more, and conformational differences are big, causes airborne electronic equipment systematical difference also very big, due to aircraft
The requirement in space and load causes the volume and weight requirement of airborne equipment very high, with the development of electronic technology, integration electricity
Subsystem has become the development trend of such aircraft airborne electronic system.
Integrated demand brings higher requirement with integrated to airborne electronic equipment system development, so that developing risk is
It improves, the lead time may increase, adversely affect to aircraft development project.In order to solve these problems, it needs to pass through number
The means of wordization emulation carry out sufficient simulating, verifying, reduce development cost, shorten the lead time, improve the maturity of product,
To effectively control development cost.
Summary of the invention
The purpose of the present invention is to propose to a kind of integrated electronic system simulators of general-purpose aircraft, are able to solve development 23
The dynamic digitalized simulation problems of portion's general-purpose aircraft integrated electronic system, can greatly shorten the lead time, be greatly lowered
Development cost, while can support the design iteration more taken turns, the maturity for newly grinding product is improved, so that wind is developed in control well
Danger.
Technical scheme is as follows: a kind of integrated electronic system simulator of general-purpose aircraft, it is characterised in that:
Including Simulation Control 101, comprehensive aobvious control emulation 102, model emulation 103, model dynamic exciting 104 and what comes into a driver's 105；Simulation Control
101 complete to adjust ginseng, mode to model emulation 103, model dynamic exciting 104, the initialization of what comes into a driver's 105, starting, stopping, dynamic
The job control of switching is completed at the same time emulation data monitoring, storage and playback function, supports according to aircraft configuration, allocation models
Which simulation model participates in emulation in emulation 103, supports the condition monitoring and daily maintenance of entire simulator；Comprehensive aobvious control is imitative
True 102 complete the display picture and logic of integrated display, are completed at the same time communication, navigation, the control panel for indicating record system
In addition the control panel emulation of the Mechatronic Systems such as power, ring control is also completed in emulation；Model emulation 103 is for emulating avionics and machine
The equipment or module of electric system；Model dynamic exciting (104) completes the dynamic exciting of model emulation 103, while driving what comes into a driver's 105
Dynamically Announce aircraft exterior scene.
Preferably, the aobvious control emulation 102 of the synthesis includes: synthesis display emulation 1021, the emulation of avionics control panel
1022 and Electromechanical Control panel emulation 1023, wherein synthesis display emulation 1021 is based on rapid prototyping using commercial tablet computer
Interface Development too development synthesis display program, avionics control panel emulation 1022 provide communication, navigation, indicate record
The control interface of avionics airborne system or module, Electromechanical Control panel emulation 1023 provide power, hydraulic, undercarriage, ring control etc.
The control interface of Mechatronic Systems or module.
Preferably, avionics control panel emulation 1022 emulates 1021 and model with synthesis display respectively with true electric interfaces
103 connection of emulation, completes the control of display picture and the control of avionics sensor；Electromechanical Control panel emulation 1023 and model emulation
103 connections, complete the control of electromechanical model.
Preferably, the model emulation 103 includes: avionics model emulation 1031 and electromechanical model emulation 1032, and can
Communicatedly connect, avionics, electromechanical model type and quantity it is configurable, the algorithm of model is configurable.
Preferably, avionics model emulation 1031 and electromechanical model emulation 1032 are communicably connected by onboard electrical interface
It connects；Avionics model emulation 1031 completes the emulation of communication, navigation and instruction recording equipment or module, and electromechanical model emulation 1032 is complete
At the emulation of the electromechanical equipments such as fuel oil, engine or module.
Preferably, the model dynamic exciting 104 includes: aircraft handling component 1041, flight simulation 1042 and flight
Environmental simulation 1043, wherein aircraft handling component 1041 is communicably connect with flight simulation 1042, completes the hand of flight simulation
Dynamic flight；Flight simulation 1042 dynamically provides flight parameter according to the model aircraft of load and shares to model emulation 103 and view
Scape 105, fight environment simulation 1043 provide meteorological natural environment information, ground communication navigation station information and air traffic information
Aircraft exterior information to model emulation 103 and what comes into a driver's 105.
Preferably, fight environment simulation (1043) completes gas epidemic disaster, the emulation of cloud natural environment, while being capable of simulated hollow
In traffic information and Communication Navigation Information, and can emulate ground communication navigation the station electromagnetic information.
Preferably, the what comes into a driver's 105 can receive and respond the order such as view angle switch of Simulation Control 101, can receive
The environmental informations such as the flight parameter of the generation of model dynamic exciting 104 and meteorology, dynamically show the external sights of aircraft, make to operate
Personnel can perceive visual in imagely flight posture, reflect the instrument instruction of card synthesis display.
9, simulator as described in claim 1, it is characterised in that: in the simulator, remove Simulation Control
101, outside what comes into a driver's 105, other modules all have the physical communications interface such as the airborne system of corresponding aircraft or the bus of module, and make
It is communicated with these communication interfaces, to realize the simulating, verifying of airborne electronic equipment system communication interface.
Present invention has the advantages that completing the maintenance management and comprehensively control of whole device by Simulation Control.Firstly,
Before l-G simulation test, the selection and initial configuration of simulation model are realized by the man-machine interface in Simulation Control, and it is imitative to complete flight
Genuine flight course planning, the initialization informations such as external environment setting；Secondly, completing the data of entire analogue system in simulation process
Monitoring and storage, and dynamic controls simulation model；Third, by playing back software, can complete emulation data after emulation
Playback and analysis.The present invention not only supports STATIC SIMULATION, but also supports dynamic simulation；Existing mathematical model simulation, and there is physics to connect
Mouth emulation.Therefore, the present invention can fully emulate, verify and analyze the mathematical model of integrated electronic system and physics connects
Mouthful, more wheel design iterations in development process can be supported, to reduce development cost well, shorten lead time, control
Developing risk.
Detailed description of the invention
Fig. 1 is system structure of the invention schematic diagram, 101 in figure: Simulation Control, 102: comprehensive aobvious control emulation, 103: model
Emulation, 104: model dynamic exciting, 105: what comes into a driver's；
Fig. 2 is the composition block diagram of the aobvious control emulation 102 of synthesis of the present invention, 1021 in figure: synthesis display emulation,
1022: the emulation of avionics control panel, 1023: the emulation of Electromechanical Control panel；
Fig. 3 is the composition block diagram of model emulation 103 of the present invention, 1031 in figure: avionics model emulation, 1032: machine
Electric model emulation；
Fig. 4 is the composition block diagram of model dynamic exciting 104 of the present invention, in figure, 1041: and aircraft handling component, 1042:
Flight simulation, 1043: fight environment simulation；
Specific embodiment
With reference to the attached drawing in the embodiment of the present invention, technical solution in the embodiment of the present invention carries out clear, complete
Ground description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.Based on this
Embodiment in invention, every other reality obtained by those of ordinary skill in the art without making creative efforts
Example is applied, shall fall within the protection scope of the present invention.
The present invention provides a kind of integrated electronic system simulator of 23 general-purpose aircrafts.As shown in Fig. 1, this is imitative
True device includes: Simulation Control 101, comprehensive aobvious control emulation 102, model emulation 103, model dynamic exciting 104 and what comes into a driver's 105.
Simulation Control 101 is connect with model emulation 103, model dynamic exciting 104 and what comes into a driver's 105 respectively by 1000M Ethernet；Model
Dynamic exciting 103 is connect by Aviation cable with model emulation 103, is connected by the udp protocol and what comes into a driver's 105 of 1000M Ethernet
It connects；Model emulation 103 is connect by Ethernet with comprehensive aobvious control emulation 102.
Simulation Control 101 is completed to the Initialize installation of its link block, starting, stopping, being moved as control management maincenter
The functions such as state control, data monitoring, data storage, data review andanalysis, operating mode switching.The operation interface of these functions by
The comprehensively control software being deployed on a work station provides.
Comprehensive aobvious control emulation 102 can complete the emulation of integrated electronic system synthesis display function and control panel.Such as
Fig. 2, comprehensive aobvious control emulation 102 include that synthesis display emulation 1021, avionics control panel emulation 1022 and Electromechanical Control panel are imitative
True 1023.Synthesis display emulation 1021 uses tablet computer using 2 Tianwan businessmans --- and for-Huawei MateBook as hardware platform, deployment is aobvious
Control processing simulation software and display Software Package For Graphic Simulation.Display control signal processing and sensor are completed in synthesis display emulation 1021
Parameter processing, and complete the driving of display picture.Simulation figure software is developed based on VAPS XT.The emulation of avionics control panel
1022 are realized in the form of simulation hardware, can complete the emulation of airborne display system and sensor control function, avionics control
Panel emulation 1022 processed is connect by USB with synthesis display emulation 1021, the information such as transmission display control.Electromechanical Control panel is imitative
True 1023 also realize that completion controls the Mechatronic Systems models such as power, ring control in the form of simulation hardware.
Model emulation 103 complete communication, navigation, monitoring, instruction record etc. avionics model emulation, be completed at the same time fuel oil,
The emulation of the Mechatronic Systems model such as engine, air-conditioning, oxygen.Such as Fig. 3, model emulation 103 includes 1031 He of avionics model emulation
Electromechanical model emulation 1032, is communicatively coupled by middleware, realizes that avionics and dynamoelectric signal are crosslinked.In model emulation 103
The model of load can be according to different aircraft type flexible configurations.The air speed of the reception model dynamic exciting offer of model emulation 103,
Highly, the data such as electromagnetic signal, dynamoelectric signal carry out dynamic simulation to drive comprehensive aobvious control emulation 102.
Model dynamic exciting 104 completes the dynamic data input of model emulation 103, comprising: aircraft handling component 1041 flies
Row emulation 1042 and fight environment simulation 1043, as shown in Figure 4.Aircraft handling component 1041 provide control stick, pedal, trim,
Man-machine interface needed for the manual drives aircraft such as throttle is communicably connect to transmit operation information with flight simulation 1042, communication
Interface is realized by the way of Ethernet.Flight simulation 1042 can receive the Initialize installation of Simulation Control 1041, comprising: flight
Plan setting, automatic/hand drive the information such as setting, fuel oil setting, the setting of aircraft initial position, original base.Flight simulation
1042 flying qualities generated share to model emulation 103 and what comes into a driver's 105 uses.Flight simulation 1042 is using based on commercial aviation
The secondary development of simulation software imports the model data of specific aircraft type.Fight environment simulation 1043 receives emulation control first
The Initialize installation of system 101 had not only included the setting of the natural environments such as temperature, wind, rain, cloud, but also including air penetration airplane information etc.
Traffic information setting.Then, model emulation 103 and what comes into a driver's are supplied to according to the related data that dynamic model calculates flight environment of vehicle
105.The radionavigation pumping signal of model emulation 103 is generated by the electromagnetic environment that fight environment simulation 1043 is simulated.Flight
The navigational route database having in environmental simulation 1043, therefore the longitude and latitude position for combining aircraft current can inquire current fly
The radionavigation station around machine generates radio signal according to the radio characteristic information of these navigation stations and completes electromagnetism
Environmental simulation.Fight environment simulation 1043 can also receive the station telecommunication setting of Simulation Control 101, complete the radio station HF, VHF
Dynamic communication excitation.
The above is a preferred embodiment of the present invention, it is noted that for those skilled in the art
For, various improvements and modifications may be made without departing from the principle of the present invention, these improvements and modifications are also considered as
Protection scope of the present invention.
Claims (9)
1. a kind of integrated electronic system simulator of general-purpose aircraft, it is characterised in that: including Simulation Control (101), synthesis
Aobvious control emulation (102), model emulation (103), model dynamic exciting (104) and what comes into a driver's (105)；Simulation Control (101) completion pair
Model emulation (103), model dynamic exciting (104), the initialization of what comes into a driver's (105), starting, stopping, dynamic adjust ginseng, pattern switching
Job control, be completed at the same time emulation data monitoring, storage and playback function, support according to aircraft configuration, allocation models emulation
(103) which simulation model participates in emulation in, supports the condition monitoring and daily maintenance of entire simulator；Comprehensive aobvious control emulation
(102) the display picture and logic for completing integrated display are completed at the same time communication, navigation, the control panel for indicating record system
In addition the control panel emulation of the Mechatronic Systems such as power, ring control is also completed in emulation；Model emulation (103) for emulate avionics and
The equipment or module of Mechatronic Systems；Model dynamic exciting (104) completes the dynamic exciting of model emulation (103), while driving view
Scape (105) Dynamically Announce aircraft exterior scene.
2. simulator as described in claim 1, it is characterised in that: the aobvious control emulation (102) of the synthesis includes: comprehensive aobvious
Show emulation (1021), avionics control panel emulation (1022) and Electromechanical Control panel emulation (1023), wherein synthesis display emulates
(1021) using commercial tablet computer, rapid prototyping Interface Development too development synthesis display program, avionics control are based on
Panel emulates (1022) and provides the control interface of communication, navigation, the avionics airborne system of instruction record or module, Electromechanical Control face
Plate emulates (1023) and provides the control interface of the Mechatronic Systems such as power, hydraulic, undercarriage, ring control or module.
3. simulator as claimed in claim 2, it is characterised in that: avionics control panel emulates (1022) really electrically to connect
Mouth is connect with synthesis display emulation (1021) and model emulation (103) respectively, completes the control of display picture and the control of avionics sensor
System；Electromechanical Control panel emulation (1023) is connect with model emulation (103), completes the control of electromechanical model.
4. simulator as described in claim 1, it is characterised in that: the model emulation (103) includes: that avionics model is imitative
Very (1031) and electromechanical model emulation (1032), and are communicatively coupled, avionics, electromechanical model type and quantity can match
It sets, the algorithm of model is configurable.
5. simulator as claimed in claim 4, it is characterised in that: avionics model emulation (1031) and electromechanical model emulation
(1032) it is communicatively coupled by onboard electrical interface；Avionics model emulation (1031) completes communication, navigation and instruction record
The emulation of equipment or module, electromechanical model emulate the emulation that (1032) complete the electromechanical equipments such as fuel oil, engine or module.
6. simulator as described in claim 1, it is characterised in that: the model dynamic exciting (104) includes: aircraft behaviour
Vertical component (1041), flight simulation (1042) and fight environment simulation (1043), wherein aircraft handling component (1041) can communicate
Ground is connect with flight simulation (1042), completes the manual flight of flight simulation；Flight simulation (1042) according to load aircraft mould
Type dynamically provides flight parameter and shares to model emulation (103) and what comes into a driver's (105), and fight environment simulation (1043) provides meteorological
The aircraft exterior information of natural environment information, ground communication navigation station information and air traffic information gives model emulation (103)
With what comes into a driver's (105).
7. simulator as claimed in claim 6, it is characterised in that: fight environment simulation (1043) completes gas epidemic disaster, cloud
Natural environment emulation, at the same can traffic information and Communication Navigation Information in simulated hollow, and ground communication guidance station can be emulated
The electromagnetic information stood.
8. simulator as described in claim 1, it is characterised in that: the what comes into a driver's (105) can receive and respond emulation control
The order such as the view angle switch of (101) is made, the environment letter such as flight parameter and meteorology of model dynamic exciting (104) generation can be received
Breath, dynamically shows the external sights of aircraft, enables an operator to perceive flight posture visual in imagely, reflects card synthesis display
Instrument instruction.
9. simulator as described in claim 1, it is characterised in that: in the simulator, except Simulation Control (101),
Outside, other modules all have the physical communications interface such as the airborne system of corresponding aircraft or the bus of module to what comes into a driver's (105), and use
These communication interfaces are communicated, to realize the simulating, verifying of airborne electronic equipment system communication interface.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201811344716.8A CN109871565A (en) | 2018-11-12 | 2018-11-12 | A kind of integrated electronic system simulator of general-purpose aircraft |
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| CN201811344716.8A CN109871565A (en) | 2018-11-12 | 2018-11-12 | A kind of integrated electronic system simulator of general-purpose aircraft |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN110781556A (en) * | 2019-10-12 | 2020-02-11 | 中航通飞研究院有限公司 | Aircraft electromagnetic environment effect simulation method |
| CN110928201A (en) * | 2019-12-26 | 2020-03-27 | 上海科梁信息工程股份有限公司 | Semi-physical test method and system for airplane avionics system |
| CN112347656A (en) * | 2020-11-17 | 2021-02-09 | 中航通飞华南飞机工业有限公司 | Simulation test device for aircraft water-drawing fire-extinguishing control system |
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| CN104050333A (en) * | 2014-06-30 | 2014-09-17 | 北京索为高科系统技术有限公司 | Distributed-type real-time comprehensive simulation system of avionics system |
| CN108196141A (en) * | 2017-11-03 | 2018-06-22 | 中航通飞研究院有限公司 | A kind of avionics system flexibility test platform and avionics integrated verification method |
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| CN104050332A (en) * | 2014-06-30 | 2014-09-17 | 北京索为高科系统技术有限公司 | Distributed-type real-time comprehensive simulation method of avionics system |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110781556A (en) * | 2019-10-12 | 2020-02-11 | 中航通飞研究院有限公司 | Aircraft electromagnetic environment effect simulation method |
| CN110781556B (en) * | 2019-10-12 | 2023-10-27 | 中航通飞华南飞机工业有限公司 | Airplane electromagnetic environment effect simulation method |
| CN110928201A (en) * | 2019-12-26 | 2020-03-27 | 上海科梁信息工程股份有限公司 | Semi-physical test method and system for airplane avionics system |
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| CN112347656A (en) * | 2020-11-17 | 2021-02-09 | 中航通飞华南飞机工业有限公司 | Simulation test device for aircraft water-drawing fire-extinguishing control system |
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Address after: 519000 1st floor, headquarters base office building, 1519 Yinwan Road, Wanchai, Xiangzhou District, Zhuhai City, Guangdong Province Applicant after: R&D INSTITUTE OF CHINA AVIATION INDUSTRY GENERAL AIRCRAFT Co.,Ltd. Address before: 519040 AVIC Tongfei industrial base, aviation industrial park, Jinwan District, Zhuhai City, Guangdong Province Applicant before: R&D INSTITUTE OF CHINA AVIATION INDUSTRY GENERAL AIRCRAFT Co.,Ltd. |
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Application publication date: 20190611 |