CN201829074U - Avionics simulation testing and training device - Google Patents
Avionics simulation testing and training device Download PDFInfo
- Publication number
- CN201829074U CN201829074U CN2010205455674U CN201020545567U CN201829074U CN 201829074 U CN201829074 U CN 201829074U CN 2010205455674 U CN2010205455674 U CN 2010205455674U CN 201020545567 U CN201020545567 U CN 201020545567U CN 201829074 U CN201829074 U CN 201829074U
- Authority
- CN
- China
- Prior art keywords
- avionics
- computing machine
- signal processing
- emulation
- testing
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
Images
Landscapes
- Management, Administration, Business Operations System, And Electronic Commerce (AREA)
Abstract
The utility model relates to an avionics simulation testing and training device. The device consists of a cockpit manipulating component, a signal processing computer, an airplane simulation computer and a simulation part, wherein the airplane simulation computer is connected with the simulation part and the signal processing computer respectively; the signal processing computer is connected with the cockpit manipulating component of the simulation part; and the simulation part is an avionics system or an avionics airborne equipment. The training device has simple and reasonable design structure; the real aviation busbar and the cockpit manipulating component, the top layer design of the avionics system, the system scheme verification, the debugging environment establishment, the co-conditioning of sub-system and equipment testing are integrated into a whole, so that all technical requirements and indexes in the simulation testing and training process can be realized, and the problems can be avoided during simultaneous testing stage or flight-test stage.
Description
Technical field
The utility model relates to a kind of simulation training device, especially a kind of avionics emulation testing trainer.
Background technology
Avionics system and aviation airborne equipment all need a simulation test platform environment from system's top layer design, comprehensive verification to system test, testing of equipment.At present, domestic special-purpose, the open-loop control systems that adopt, the platform environment of the simple functions of building rapidly under the situation of and time weak point few at manpower more.
At present, along with the complexity raising of avionic device, just more and more higher to the requirement that avionics system and avionics airborne equipment design, verify, test, test.Yet existing analogue system or test macro also do not have to provide complete, integrated plateform system.Design, exploitation for the avionics airborne equipment do not have available emulation platform and support Aided Design, exploitation; The test of avionics system, test are confined to minority, subsystem commonly used more, adopt the mode of independent experiment and test to realize for most subsystems more, can't realize the target of compbined test and test, Combined Trials, the stage of taking a flight test so just having occurred goes wrong many, the design system complexity, investigation long situation fault-time.
The utility model content
At the weak point that exists in the above-mentioned technology, the utility model provides a kind of true aviation bus and passenger cabin manipulation assembly, the design of avionics system top layer, system schema checking, debugging enironment structure, subsystem combined test, testing of equipment set is the avionics emulation testing trainer of one.
For achieving the above object, the utility model provides a kind of avionics emulation testing trainer, handling assembly, signal Processing computing machine, flight simulation computing machine and emulation by passenger cabin partly constitutes, described flight simulation computing machine is connected with described emulation part and described signal Processing computing machine respectively, and described signal Processing computing machine is handled assembly with described emulation part and described passenger cabin respectively and is connected.
Described emulation partly is avionics system or avionics airborne equipment.
Described signal Processing computing machine is connected with signal input-output device, described signal input-output device is handled assembly, avionics system or avionics airborne equipment with described passenger cabin and is connected, and described signal input-output device is made of aviation bus signals, analog signals input-output device and discrete magnitude signal input-output device.
Be provided with in the described signal Processing computing machine and be used to gather the interactive interface that described passenger cabin is handled assembly and described emulation part.
Described signal Processing computing machine is signals collecting and signal excitation computing machine.
Compared with prior art, the utlity model has following advantage:
The avionics emulation testing trainer that the utility model provides, handling assembly, signal Processing computing machine, flight simulation computing machine and emulation by passenger cabin partly constitutes, the flight simulation computing machine is connected with emulation part and signal Processing computing machine respectively, the signal Processing computing machine is handled assembly with emulation part passenger cabin and is connected, and emulation partly is POP analogue system, avionics system or avionics airborne equipment.The utility model project organization advantages of simple, true aviation bus and passenger cabin manipulation assembly, the design of avionics system top layer, system schema checking, debugging enironment structure, subsystem combined test, testing of equipment set are one, can realize all technical requirements and index in the emulation testing training process, and can avoid going wrong at Combined Trials or the stage of taking a flight test.
Description of drawings
Fig. 1 is a structured flowchart of the present utility model;
Fig. 2 is an embodiment block diagram of the present utility model;
Fig. 3 is another embodiment block diagram of the present utility model;
Fig. 4 is an another embodiment block diagram of the present utility model.
The main element symbol description is as follows:
1 flight simulation computing machine 2POP analogue system
3 signal Processing computing machines, 4 passenger cabins are handled assembly
5 avionics airborne equipments, 6 signal input-output device
7 emulation parts, 8 signals collecting and signal excitation computing machine
Embodiment
For clearer statement the utility model, the utility model will be further described below in conjunction with accompanying drawing.
As shown in Figure 1, the utility model provides a kind of avionics emulation testing trainer, constitute by flight simulation computing machine 1, signal Processing computing machine 3, passenger cabin manipulation assembly 4 and emulation part 7, wherein, flight simulation computing machine 1 is connected with emulation part 7 and signal Processing computing machine 3 by ethernet network respectively, signal Processing computing machine 3 is connected with emulation part 7, and signal Processing computing machine 3 is also handled assembly 4 by USB interface or signal input-output device 6 with passenger cabin and is connected.In signal Processing computing machine 3, be provided with and be used to gather the interactive interface that passenger cabin is handled assembly 4 and emulation part 7.Emulation partly is POP analogue system, avionics system or avionics airborne equipment.
The flight simulation computing machine is a core of the present utility model, partly forms emulation, test loop by interface and passenger cabin, emulation, thereby forms a cover avionics simulation test platform.The flight simulation computing machine provides aircraft each module data, for the avionics airborne equipment provides driving source, for the POP simulation computer provides data source, forms closed loop by passenger cabin collection and avionics/non-avionics signals collecting.Data-interface comprises network, ARINC429, MIL-STD-1553, AFDX, reflective memory etc., and signal excitation comprises D/A, DO, RVDT etc., and signals collecting comprises ARINC429, MIL-STD-1553, A/D, DI, LVDT etc.
Passenger cabin is handled assembly and is comprised manipulation assemblies such as throttle lever, jociey stick, pedal, wing flap/slat joystick, flap joystick, control wheel.
The flight simulation computing machine can be finished the overall process of taking off, cruise, land of aircraft based on the general-purpose aircraft realistic model.In the aircraft flight process, export the flight parameter data such as positional information, radio navigation information, engine data of atmospheric engine data, atmospheric environment data, aircraft rudder surface position, flight attitude information, various coordinate systems in real time; Can make amendment to parameters such as earth model, pilot's input, way point, flight management, fuel oil, undercarriage, engines simultaneously; And have robot pilot, automatically flight, automatic throttle, a flight control function such as maintenance highly.
It mainly is the collection of throttle lever, jociey stick, pedal, wing flap/slat joystick, flap joystick, control wheel in the passenger cabin etc. being handled assembly that passenger cabin is handled the assembly collection, and acquired signal is sent in the flight simulation computer model.Avionics airborne equipment interactive interface is reception and the transmission to ARINC429, MIL-STD-1553, AFDX bus signals, and the collection and the excitation of various simulating signal, digital quantity signal, angle signal, finishes the needs to avionics testing of equipment, checking.
As shown in Figure 2, the utility model provides a kind of avionics emulation testing trainer, partly constitute by flight simulation computing machine 1, signal Processing computing machine, passenger cabin manipulation assembly 4 and emulation, flight simulation computing machine 1 is connected with emulation part and signal Processing computing machine by ethernet network respectively, and the signal Processing computing machine is also handled assembly 4 by USB interface or signal input-output device 6 with passenger cabin and is connected.Wherein, emulation partly is POP analogue system 2, and POP analogue system 2 is connected with flight simulation computing machine 1, and the POP analogue system is mainly used in design, the comprehensive verification of design of avionics system top layer and Comprehensive Control display technique.Flight Simulation System can be exported needed flight parameter of POP analogue system and instrumented data, and signals collecting and signal excitation computing machine are finished and gathered analog capsule cabin manipulation component signals, send flight Simulation System to.
As shown in Figure 3, the utility model provides a kind of avionics emulation testing trainer, partly constitute by flight simulation computing machine 1, signal Processing computing machine 3, passenger cabin manipulation assembly 4 and emulation, flight simulation computing machine 1 is connected with the signal Processing computing machine by ethernet network respectively, the signal Processing computing machine is also handled assembly 4 by USB interface or signal input-output device 6 with passenger cabin and is connected, and the signal Processing computing machine also is connected with avionics airborne equipment 5 by signal input-output device 6.Wherein, avionics airborne equipment 5 is the emulation part, and the avionics airborne equipment mainly is real avionics airborne equipment, and usage platform carries out Equipment Inspection.Be provided with the interactive interface that is used to gather passenger cabin manipulation assembly and avionics airborne equipment in the signal Processing computing machine, this signal Processing computing machine is signals collecting and signal excitation computing machine 8.
As shown in Figure 4, the utility model provides a kind of avionics emulation testing trainer, partly constitute by flight simulation computing machine 1, signal Processing computing machine, passenger cabin manipulation assembly 4 and emulation, flight simulation computing machine 1 is connected with emulation part and signal Processing computing machine by ethernet network respectively, the signal Processing computing machine is also handled assembly 4 by USB interface or signal input-output device 6 with passenger cabin and is connected, and signal input-output device 6 also is connected with avionics airborne equipment 5.Wherein, emulation partly is POP analogue system 2, POP analogue system 2 is connected with flight simulation computing machine 1, perhaps link to each other with the signal Processing computing machine by signal input-output device 6, the POP analogue system is mainly used in design, the comprehensive verification of design of avionics system top layer and Comprehensive Control display technique.Be provided with the interactive interface that is used to gather passenger cabin manipulation assembly and POP analogue system in the signal Processing computing machine, this signal Processing computing machine is signals collecting and signal excitation computing machine 8.Signals collecting is connected with signal input-output device 6 with signal excitation computing machine 8, signal input-output device 6 is handled assembly 4 with passenger cabin and is connected, and signal input-output device is made of analog signals input-output device and discrete magnitude signal input-output device.
With the crosslinked test of comprehensive avionics system the time, the flight simulation computing machine provides various flight parameters, environmental parameter and navigation signal, finish flight parameter to the pumping signal conversion by signals collecting and signal excitation computing machine, these pumping signals send aircraft ADC, AHC, IRS, RNAV, ISI subsystem to the most at last.Synchronous signal is gathered with the signal excitation computing machine will gather control signal and bus signals, analog quantity, discrete magnitude, pass to flight Simulation System after the switching signal.
Major function of the present utility model requires as follows:
1, has the function of the characteristic of general-purpose aircraft platform being carried out emulation;
2, has the function of the external environment condition of general-purpose aircraft being carried out dynamic similation;
3, have the demonstration of general-purpose aircraft flying instruments, various control button or assembly copying;
4, support auxiliary avionics system top layer design, comprehensive verification;
5, has avionics system compbined test function;
6, support the design of avionics airborne equipment, exploitation, test, various test stages environmental requirement;
7, support the standard passenger cabin to handle assembly.
More than disclosed only be several specific embodiment of the present utility model, still, the utility model is not limited thereto, any those skilled in the art can think variation all should fall into protection domain of the present utility model.
Claims (5)
1. avionics emulation testing trainer, handling assembly, signal Processing computing machine, flight simulation computing machine and emulation by passenger cabin partly constitutes, it is characterized in that, described flight simulation computing machine is connected with described emulation part and described signal Processing computing machine respectively, and described signal Processing computing machine is handled assembly with described emulation part and described passenger cabin respectively and is connected.
2. a kind of avionics emulation testing trainer as claimed in claim 1 is characterized in that described emulation partly is avionics system or avionics airborne equipment.
3. a kind of avionics emulation testing trainer as claimed in claim 2, it is characterized in that, described signal Processing computing machine is connected with signal input-output device, described signal input-output device is handled assembly, avionics system or avionics airborne equipment with described passenger cabin and is connected, and described signal input-output device is made of aviation bus signals, analog signals input-output device and discrete magnitude signal input-output device.
4. a kind of avionics emulation testing trainer as claimed in claim 1 is characterized in that, is provided with in the described signal Processing computing machine to be used to gather the interactive interface that described passenger cabin is handled assembly and described emulation part.
5. as any described a kind of avionics emulation testing trainer in the claim 1 to 4, it is characterized in that described signal Processing computing machine is signals collecting and signal excitation computing machine.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010205455674U CN201829074U (en) | 2010-09-28 | 2010-09-28 | Avionics simulation testing and training device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010205455674U CN201829074U (en) | 2010-09-28 | 2010-09-28 | Avionics simulation testing and training device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201829074U true CN201829074U (en) | 2011-05-11 |
Family
ID=43967596
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2010205455674U Expired - Lifetime CN201829074U (en) | 2010-09-28 | 2010-09-28 | Avionics simulation testing and training device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201829074U (en) |
Cited By (18)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102968059A (en) * | 2012-08-10 | 2013-03-13 | 中国商用飞机有限责任公司 | Aircraft landing gear simulator |
| CN103116287A (en) * | 2013-01-22 | 2013-05-22 | 中国民航大学 | Avionics equipment running environment dynamic simulating device and method |
| 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 |
| CN104360115A (en) * | 2014-11-28 | 2015-02-18 | 成都航天通信设备有限责任公司 | Airborne avionics information simulator |
| CN105373023A (en) * | 2015-11-24 | 2016-03-02 | 中国航空工业集团公司沈阳飞机设计研究所 | Avionics integration test integrated control assembly |
| CN105372530A (en) * | 2015-11-24 | 2016-03-02 | 中国航空工业集团公司沈阳飞机设计研究所 | Single test debugging system with real-time simulation test capability |
| CN105590495A (en) * | 2016-03-18 | 2016-05-18 | 中国直升机设计研究所 | Reconfigurable avionics system training simulator |
| CN106527401A (en) * | 2016-11-30 | 2017-03-22 | 中国航空工业集团公司沈阳飞机设计研究所 | Flight control test automated testing system |
| CN106586029A (en) * | 2016-12-28 | 2017-04-26 | 中国航空工业集团公司西安飞机设计研究所 | Test system of high-lift control system |
| CN107886800A (en) * | 2017-11-28 | 2018-04-06 | 浙江中航通飞研究院有限公司 | A kind of aircraft cockpit avionics simulation system of people in the loop |
| CN107944193A (en) * | 2017-12-15 | 2018-04-20 | 四川汉科计算机信息技术有限公司 | Avionics semi-matter simulating 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 |
| CN108646705A (en) * | 2018-04-16 | 2018-10-12 | 西安飞机工业（集团）有限责任公司 | A kind of airplane ground test interconnection of signals TT＆C system |
| CN109192037A (en) * | 2018-07-28 | 2019-01-11 | 国营芜湖机械厂 | A kind of avionics joint-trial environmental technology arrangement demo system based on VR |
| CN109855651A (en) * | 2018-11-12 | 2019-06-07 | 中航通飞研究院有限公司 | The ground testing system and test method of modern aircraft radio communication navigation system |
| CN112270859A (en) * | 2020-10-20 | 2021-01-26 | 上海航翼高新技术发展研究院有限公司 | Aircraft avionics joint debugging testing device based on cooperative robot and testing method thereof |
| CN113096484A (en) * | 2021-04-15 | 2021-07-09 | 中国人民解放军空军军医大学 | Design method of space directional obstacle flight simulation equipment |
| CN114486310A (en) * | 2021-12-31 | 2022-05-13 | 中国航空工业集团公司西安飞机设计研究所 | Dynamic simulation comprehensive test system and method for aircraft electromechanical management system |
-
2010
- 2010-09-28 CN CN2010205455674U patent/CN201829074U/en not_active Expired - Lifetime
Cited By (25)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102968059A (en) * | 2012-08-10 | 2013-03-13 | 中国商用飞机有限责任公司 | Aircraft landing gear simulator |
| CN102968059B (en) * | 2012-08-10 | 2016-07-13 | 中国商用飞机有限责任公司 | Undercarriage simulator |
| CN103116287A (en) * | 2013-01-22 | 2013-05-22 | 中国民航大学 | Avionics equipment running environment dynamic simulating device and method |
| CN103456202B (en) * | 2013-09-05 | 2016-01-06 | 上海蔚翼航空科技有限公司 | A kind of simulation equipment based on Aircraft Flight Test training and system thereof |
| 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 |
| CN104360115A (en) * | 2014-11-28 | 2015-02-18 | 成都航天通信设备有限责任公司 | Airborne avionics information simulator |
| CN104360115B (en) * | 2014-11-28 | 2017-06-30 | 成都航天通信设备有限责任公司 | Airborne avionics information simulation device |
| CN105372530A (en) * | 2015-11-24 | 2016-03-02 | 中国航空工业集团公司沈阳飞机设计研究所 | Single test debugging system with real-time simulation test capability |
| CN105373023A (en) * | 2015-11-24 | 2016-03-02 | 中国航空工业集团公司沈阳飞机设计研究所 | Avionics integration test integrated control assembly |
| CN105590495A (en) * | 2016-03-18 | 2016-05-18 | 中国直升机设计研究所 | Reconfigurable avionics system training simulator |
| CN105590495B (en) * | 2016-03-18 | 2019-05-07 | 中国直升机设计研究所 | A kind of restructural avionics system training simulators |
| CN106527401A (en) * | 2016-11-30 | 2017-03-22 | 中国航空工业集团公司沈阳飞机设计研究所 | Flight control test automated testing system |
| CN106527401B (en) * | 2016-11-30 | 2023-09-05 | 中国航空工业集团公司沈阳飞机设计研究所 | Automatic test system for flight control test |
| CN106586029A (en) * | 2016-12-28 | 2017-04-26 | 中国航空工业集团公司西安飞机设计研究所 | Test system of high-lift control system |
| CN106586029B (en) * | 2016-12-28 | 2019-06-11 | 中国航空工业集团公司西安飞机设计研究所 | A kind of test macro of promotion Force control 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 |
| CN107886800A (en) * | 2017-11-28 | 2018-04-06 | 浙江中航通飞研究院有限公司 | A kind of aircraft cockpit avionics simulation system of people in the loop |
| CN107944193A (en) * | 2017-12-15 | 2018-04-20 | 四川汉科计算机信息技术有限公司 | Avionics semi-matter simulating system |
| CN108646705A (en) * | 2018-04-16 | 2018-10-12 | 西安飞机工业（集团）有限责任公司 | A kind of airplane ground test interconnection of signals TT＆C system |
| CN109192037A (en) * | 2018-07-28 | 2019-01-11 | 国营芜湖机械厂 | A kind of avionics joint-trial environmental technology arrangement demo system based on VR |
| CN109855651A (en) * | 2018-11-12 | 2019-06-07 | 中航通飞研究院有限公司 | The ground testing system and test method of modern aircraft radio communication navigation system |
| CN109855651B (en) * | 2018-11-12 | 2023-10-27 | 中航通飞华南飞机工业有限公司 | Ground test system and test method for modern aircraft radio communication navigation system |
| CN112270859A (en) * | 2020-10-20 | 2021-01-26 | 上海航翼高新技术发展研究院有限公司 | Aircraft avionics joint debugging testing device based on cooperative robot and testing method thereof |
| CN113096484A (en) * | 2021-04-15 | 2021-07-09 | 中国人民解放军空军军医大学 | Design method of space directional obstacle flight simulation equipment |
| CN114486310A (en) * | 2021-12-31 | 2022-05-13 | 中国航空工业集团公司西安飞机设计研究所 | Dynamic simulation comprehensive test system and method for aircraft electromechanical management system |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN201829074U (en) | Avionics simulation testing and training device | |
| CN107942720B (en) | Portable ground online flight simulation system | |
| CN106598032B (en) | A kind of test macro of automatic flight control system | |
| CN108983756B (en) | Avionics flight control system ground comprehensive debugging and verification platform | |
| CN108053714B (en) | Multi-rotor unmanned aerial vehicle based on polling transmission line makes an inspection tour operation simulation training system | |
| CN103456202B (en) | A kind of simulation equipment based on Aircraft Flight Test training and system thereof | |
| CN111176999B (en) | Test platform construction method and test method of unmanned aerial vehicle flight control management software | |
| CN102779436B (en) | Collaborative and intelligent training method for aircraft maintenance | |
| CN107991903A (en) | Fly control semi-matter simulating system | |
| CN109933047B (en) | Joint reliability test profile construction method of software and hardware hybrid system | |
| CN102750849B (en) | Cooperative intelligent mechanical maintenance simulation machine | |
| CN105825013A (en) | Aviation command guaranty optimization method based on discrete event system | |
| CN106094566A (en) | A kind of method for low cost universal ground experiment simulation carrier aircraft system | |
| CN105116758A (en) | Simulation method of industrial electronic embedded system | |
| CN110060541B (en) | Simulation training system for airplane navigation posture equipment | |
| CN205508229U (en) | Aircraft engine semi physical flight simulator | |
| CN109871565A (en) | A kind of integrated electronic system simulator of general-purpose aircraft | |
| CN107293186A (en) | A kind of inertial navigation real-time emulation system of training simulators | |
| CN203013017U (en) | Distributed-type non-avionic simulation excitation system | |
| CN112084630B (en) | Identification test method and system for D-level flight simulation training equipment | |
| CN109992897B (en) | Radio altimeter simulation method for ground proximity warning equipment | |
| CN112612297A (en) | Airworthiness verification system and method for civil aircraft automatic flight control system | |
| CN113050583A (en) | Flight control system ground test platform and test method thereof | |
| CN113066315B (en) | Scene capture analysis method for civil aircraft approach landing stage flight safety | |
| CN113777980B (en) | Simulation test device and external equipment for airplane cabin command control system |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CX01 | Expiry of patent term | ||
| CX01 | Expiry of patent term |
Granted publication date: 20110511 |