CN104064071A - Small fixed flight training device system - Google Patents

Small fixed flight training device system Download PDF

Info

Publication number
CN104064071A
CN104064071A CN201410281026.8A CN201410281026A CN104064071A CN 104064071 A CN104064071 A CN 104064071A CN 201410281026 A CN201410281026 A CN 201410281026A CN 104064071 A CN104064071 A CN 104064071A
Authority
CN
China
Prior art keywords
flight
simulation
program
instrument
simulation framework
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.)
Pending
Application number
CN201410281026.8A
Other languages
Chinese (zh)
Inventor
杨实
王治宇
白杨
杨正
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Zhuhai Xiangyi Aviation Technology Co Ltd
Original Assignee
Zhuhai Xiangyi Aviation Technology Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Zhuhai Xiangyi Aviation Technology Co Ltd filed Critical Zhuhai Xiangyi Aviation Technology Co Ltd
Priority to CN201410281026.8A priority Critical patent/CN104064071A/en
Publication of CN104064071A publication Critical patent/CN104064071A/en
Pending legal-status Critical Current

Links

Landscapes

  • Management, Administration, Business Operations System, And Electronic Commerce (AREA)

Abstract

The invention discloses a small fixed flight training device system which comprises a first simulation host, a second simulation host in communication with the first simulation host and a visual image displayer, wherein flight simulation software is arranged in the first simulation host and used for acquiring the input data of a flight controlling device for flight simulation, generating visual images of flight, and calculating corresponding flight parameters, a flight parameter acquisition program is further arranged in the first simulation host and used for acquiring the flight parameters to drive devices such as a simulation instrument, a teacher management client program is arranged in the second simulation host and used for acquiring the flight parameters from the server side of a visual image program directly, displaying flight states and enabling a teacher to evaluate the flight condition, a G1000 liquid crystal comprehensive instrument simulation program is further arranged in the second simulation host and used for displaying main flight parameters and navigation data, and the visual image displayer is connected with the first simulation host and used for displaying the visual images. The small fixed flight training device system is designed in a modular mode and simple in structure, and can be widely applied to various flight training devices similar to airplanes by changing the overall arrangement of a driving panel.

Description

A kind of small-sized fixedly flight training device system
Technical field
The present invention relates to simulated training field, particularly a kind of small-sized fixedly flight training device system.
Background technology
Flight training device is to utilize the exercise equipment for pilot's training of virtual reality technology and emulation technology exploitation.Traditional low side flight training device is often used Virtual Cockpit System, and the equipment such as its flying instruments, control lever, switch are all used the display screen with touch function.This training aids is difficult to accomplish dimensionally consistent with true aircraft cabin, and the validity of pilot in visual experience is poor; Chain of command at flight simulation also lacks the feel consistent with prototype, lacks the operating experience in basic sense of touch.The polylith display screen that training aids based on Virtual Cockpit System is used in addition, need to, by extra computer drives, increase system cost.And high-end flight training device is used prototype scrap build in a large number, the connection complex of its instrument, actuation means etc., interface circuit is difficult to unified, has not only strengthened maintenance difficulties, has also increased cost.
Summary of the invention
For addressing the above problem, the object of the present invention is to provide a kind of small-sized fixedly flight training device system, whole system is based on modular design, its emulation instrument system is independent separately, actual disposition that can complete simulation type, and carry out optimum, the simplest layout, promote the reliability of simulation, and its cost is lower, be convenient to safeguard.
The present invention solves the technical scheme that its problem adopts:
A small-sized fixedly flight training device system, comprising:
(1) simulation framework one,
In it, there are flight simulation software, what comes into a driver's program and flight parameter capture program, wherein,
Described flight simulation software carries out flight simulation for gathering the input data of flight actuation means, generates the scenery picture of flight course, and calculates corresponding flight parameter;
Described what comes into a driver's program is for receiving and show the scenery picture of flight simulation Software Create;
Described flight parameter capture program is for gathering the flight parameter drawing from flight simulation Software simulation calculation, with driving simulation equipment;
(2) with the simulation framework two of simulation framework one communication connection,
In it, there is management of teachers's client-side program, what comes into a driver's program in described simulation framework one is set up the service end that has management of teachers's client-side program, management of teachers's client-side program is used for directly from then on service end and obtains flight parameter, automatically flight parameter is assessed, completed aircraft parameter setting, location, position, airport and system failure setting;
Also, there is G1000 liquid crystal navigation instrument simulator program, for showing main flight parameter and navigation map information;
(3) visual display device, is connected with simulation framework one, for passing through scenery picture corresponding to what comes into a driver's program display;
(4) emulation G1000 liquid crystal integrative instrument, is connected with simulation framework two, for showing corresponding what comes into a driver's information by G1000 liquid crystal navigation instrument simulator program.
Above-described whole training aids system adopts two main frames to connect corresponding operating equipment and emulation instrument, wherein, main frame one carries out flight simulation and calculates output scenery picture, and gather flight parameter driving simulation instrument by usb bus, main frame two is by TCP/IP network collection flight parameter, driving simulation G1000 liquid crystal integrative instrument.
Further, described flight actuation means at least comprises operating rod, pin rudder, throttle and mixing ratio bar, described emulator comprises machinery instrument and switch panel, described machinery instrument at least comprises airspeed indicator, height indicator, horizon instrument, compass, described switch panel comprises headlamp switch, wing flap control panel, trim wheel, and described actuation means, machinery instrument and switch panel communicate to connect with simulation framework one after connecting HUB by usb bus.
Further, described airspeed indicator, height indicator, horizon instrument, compass are independent HID equipment.
Described simulation framework one communicates to connect by USB interface with current game controller protocol and actuation means, emulation instrument, between described simulation framework one and simulation framework two, with ICP/IP protocol, communicates to connect.Actuation means and emulation instrument adopt game console agreement to realize the moving design of free drive.Be arranged in the flight simulation software communication that G1000 liquid crystal on simulation framework two navigation integrative instrument and management of teachers's client software adopt ICP/IP protocol and simulation framework one.Above two kinds of interfaces are conventional interfaces, and conventional network service is consistent, and is conducive to the modular design of training aids, shorten the R&D cycle and save cost.
Further, described machinery instrument adopts high frequency refresh rate to guarantee the accurate renewal of machinery instrument, and described switch panel adopts low frequency refresh rate or message-driven mode to guarantee that the switching signal on switch panel is accurately identified.Because instrument, switch panel require inconsistently to sensitivity, therefore, adopt the mode refreshing of distinguishing, the one, reduced workload, the 2nd, promoted operational efficiency.
The invention has the beneficial effects as follows:
The present invention adopts a kind of small-sized fixedly flight training device system, and whole training aids designs according to the ratio of cessna172R driving cabin 1:1.One-piece construction is simple, no matter is hardware or software, all takes modular design, is conducive to reduce overlapping development and the customizedization service to different clients; Hardware configuration is corresponding fairly simple, is conducive to orientation and reduces costs, and the simple corresponding software of hardware configuration is also relatively simple, and modular Software for Design is not only beneficial to the realization of control, and daily servicing is also fairly simple.The making of hardware can adopt conventional technique and material, fully reduces costs.
Accompanying drawing explanation
Below in conjunction with accompanying drawing and example, the invention will be further described.
Fig. 1 is one-piece construction schematic diagram of the present invention;
Fig. 2 is principle schematic in kind of the present invention.
Embodiment
Shown in Fig. 1, the invention provides a kind of small-sized fixedly flight training device system, comprising:
(1) simulation framework one,
In it, there are flight simulation software, what comes into a driver's program and flight parameter capture program, wherein,
Described flight simulation software carries out flight simulation for gathering the input data of flight actuation means, generates the scenery picture of flight course, and calculates corresponding flight parameter;
Described what comes into a driver's program is for receiving and show the scenery picture of flight simulation Software Create;
Described flight parameter capture program is for gathering the flight parameter drawing from flight simulation Software simulation calculation, with driving simulation equipment;
(2) with the simulation framework two of simulation framework one communication connection,
Inside there is management of teachers's client-side program, what comes into a driver's program in described simulation framework one is set up the service end that has management of teachers's client-side program, management of teachers's client-side program is used for directly from then on service end and obtains flight parameter, and carry out the demonstration of state of flight, realize teacher flight condition is assessed, teacher also can arrange aircraft state, initial position etc. by management of teachers's client-side program;
Also, there is G1000 liquid crystal integrative instrument simulator program, for the demonstration of main flight parameter and navigation data;
(3) visual display device, is connected with simulation framework one, for passing through scenery picture corresponding to what comes into a driver's program display;
(4) emulation G1000 liquid crystal integrative instrument, is connected with simulation framework two, for showing corresponding what comes into a driver's information by G1000 liquid crystal navigation instrument simulator program.
Due to simulation framework one operation is acquisition driver, what comes into a driver's program, real-time processing requirements to data is higher, and simulation framework two operations is management of teachers's client-side program, G1000 liquid crystal navigation instrument simulator program, complete the subsequent treatment of corresponding data, therefore, processing requirements is lower.So in the hardware configuration of simulation framework one and simulation framework two, simulation framework one need to adopt higher configuration, and second simulation framework can adopt relatively low configuration.In the present invention, simulation framework one adopt i7(or more than) CPU all can, and second simulation framework adopts i5 (or more than) CPU.Reasonably dispose to be beneficial to fully and reduce costs.
Because be easy flight training system, therefore, in the present invention, described actuation means at least comprises operating rod, pin rudder, throttle and mixing ratio bar, described emulator comprises machinery instrument and switch panel, described machinery instrument at least comprises airspeed indicator, height indicator, horizon instrument, compass, and described switch panel comprises headlamp switch, wing flap control panel, trim wheel, and described actuation means, machinery instrument and switch panel communicate to connect with simulation framework one after connecting HUB by usb bus.The present invention is when design actuation means, machinery instrument, switch panel, the one, meet the key link that flight is trained, the 2nd, when global design, guarantee the promptness that actuation means, machinery instrument, switch panel are processed with the real-time of communicating by letter and the simulation framework of simulation framework one.Therefore, the present invention communicates by letter with simulation framework one after adopting usb bus to connect HUB.And adopt HUB as transponder, and guaranteed that all transmission do not interfere with each other, even a certain transmission line failure, other transmission lines are normally operation still.
The machinery instrument that this flight training system adopts comprises four kinds of airspeed indicators, height indicator, horizon instrument, compass, in order better to communicate by letter with simulation framework one, is all designed to independent HID equipment.So not only can expand on the simulator of other types and use, also guarantee the smooth and easy of communication.For simplified design, airspeed indicator, height indicator and compass only have a pointer demand motive in physical construction.The load of pointer is very little, there is no other extra drive mechanisms, and for Small General Aircraft, air speed, highly, the variation in course is more slow, less demanding to the rotating speed of electric pointer, so can select common decelerating step motor.
The present invention adopts above design by airspeed indicator, height indicator, horizon instrument, compass, can better communicate by letter with simulation framework, also can expand on the simulator of other types and use.
Simulation framework one can be used the video card of 3 screen outputs, completes the splicing of 3 passage scenery pictures by video fusion technology, realizes 180 ° of ring curtain effects; On training aids cheaply, owing to only requiring single pass scenery picture, therefore, it can only use the video card of single screen to complete single pass effect.
In the present invention, described simulation framework one, with current game controller protocol and the communication connection of flight actuation means, communicates to connect with Transmission Control Protocol between described simulation framework one and simulation framework two.Actuation means and emulation instrument adopt game console agreement can realize the moving design of free drive.Be arranged in the flight simulation software communication that G1000 liquid crystal navigation instrument simulator program on simulation framework two and management of teachers's client software adopt ICP/IP protocol and simulation framework one.Above two kinds of interfaces are conventional interfaces, and conventional network service is consistent, and is conducive to the modular design of training aids, shorten the R&D cycle and save cost.
For machinery instrument and switch panel, the division of high speed, low speed need to be carried out to these equipment, to guarantee targetedly accuracy.The real-time property that machinery instrument needs is stronger, and for switch panel, does not want too high real-time.Therefore, described machinery instrument adopts high frequency refresh rate to upgrade to guarantee the precision of machinery instrument, can be decided to be the refresh rate of 10 times per second, described switch panel adopts low frequency refresh rate (as the refresh rate of 2-4 time per second) or message-driven mode to guarantee that the switching signal on switch panel is accurately identified, message-driven mode must add verification scheme, guarantees that switching manipulation can be identified accurately.
Shown in Fig. 2, whole system comprises main frame one and main frame two, by bridge, can operate management of teachers's client-side program, and visual display device can show state of flight, and teacher can observe directly correspondence image.In the present invention, because emulation instrument adopts modular design, for using similar instrumentation but layout different dissimilar type, the design of only changing bridge front panel can complete the compatible design of different type of machines training aids.
Above design of the present invention, simple in structure, different parts have versatility widely, can apply in different flight training device, fully reduce costs.
The above, be preferred embodiment of the present invention, and the present invention is not limited to above-mentioned embodiment, as long as it reaches technique effect of the present invention with identical means, all should belong to protection scope of the present invention.

Claims (5)

1. a small-sized fixedly flight training device system, is characterized in that, comprising:
(1) simulation framework one,
In it, there are flight simulation software, what comes into a driver's program and flight parameter capture program, wherein,
Described flight simulation software carries out flight simulation for gathering the input data of flight actuation means, generates the scenery picture of flight course, and calculates corresponding flight parameter;
Described what comes into a driver's program is for receiving and show the scenery picture of flight simulation Software Create;
Described flight parameter capture program is for gathering the flight parameter drawing from flight simulation Software simulation calculation, with driving simulation equipment;
(2) with the simulation framework two of simulation framework one communication connection,
In it, there is management of teachers's client-side program, what comes into a driver's program in described simulation framework one is set up the service end that has management of teachers's client-side program, management of teachers's client-side program is used for directly from then on service end and obtains flight parameter, automatically flight parameter is assessed, completed aircraft parameter setting, location, position, airport and system failure setting;
Also, there is G1000 liquid crystal navigation instrument simulator program, for showing main flight parameter and navigation map information;
(3) visual display device, is connected with simulation framework one, for passing through scenery picture corresponding to what comes into a driver's program display;
(4) emulation G1000 liquid crystal integrative instrument, is connected with simulation framework two, for showing corresponding what comes into a driver's information by G1000 liquid crystal navigation instrument simulator program.
2. small-sized fixedly flight training device system according to claim 1, it is characterized in that, described flight actuation means at least comprises operating rod, pin rudder, throttle and mixing ratio bar, described emulator comprises machinery instrument and switch panel, described machinery instrument at least comprises airspeed indicator, height indicator, horizon instrument, compass, described switch panel comprises headlamp switch, wing flap control panel, trim wheel, and described actuation means, machinery instrument and switch panel communicate to connect with simulation framework one after connecting HUB by usb bus.
3. small-sized fixedly flight training device system according to claim 2, is characterized in that, described airspeed indicator, height indicator, horizon instrument, compass are independent HID equipment.
4. small-sized fixedly flight training device system according to claim 2, it is characterized in that, described simulation framework one, with current game controller protocol and the communication connection of flight actuation means, communicates to connect with Transmission Control Protocol between described simulation framework one and simulation framework two.
5. small-sized fixedly flight training device system according to claim 2, it is characterized in that, described machinery instrument adopts high frequency refresh rate to guarantee the accurate renewal of machinery instrument, and described switch panel adopts low frequency refresh rate or message-driven mode to guarantee that the switching signal on switch panel is accurately identified.
CN201410281026.8A 2014-06-20 2014-06-20 Small fixed flight training device system Pending CN104064071A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410281026.8A CN104064071A (en) 2014-06-20 2014-06-20 Small fixed flight training device system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410281026.8A CN104064071A (en) 2014-06-20 2014-06-20 Small fixed flight training device system

Publications (1)

Publication Number Publication Date
CN104064071A true CN104064071A (en) 2014-09-24

Family

ID=51551755

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201410281026.8A Pending CN104064071A (en) 2014-06-20 2014-06-20 Small fixed flight training device system

Country Status (1)

Country Link
CN (1) CN104064071A (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104809935A (en) * 2015-05-13 2015-07-29 中国航空工业集团公司沈阳飞机设计研究所 Simulation training method for special situation fault of unmanned aerial vehicle and system thereof
WO2017107323A1 (en) * 2015-12-22 2017-06-29 成都艾尔伯特科技有限责任公司 Flight simulation entertainment experience apparatus
CN107067873A (en) * 2016-11-25 2017-08-18 上海航空电器有限公司 The flight simulation flight Horizon table controlled based on CAN
CN109062629A (en) * 2018-07-13 2018-12-21 成都泛美视界科技有限公司 A kind of performance optimization method of flight simulation software
CN109243243A (en) * 2018-10-08 2019-01-18 卓尔飞机制造(武汉)有限公司 Flight simulation simulation training system and its Training Methodology
CN110164236A (en) * 2019-05-28 2019-08-23 四川信息职业技术学院(广元无线电技工学校) Multi-functional unmanned plane teaching test case
CN110335519A (en) * 2019-07-16 2019-10-15 上海卡索航空科技有限公司 A kind of 172 general-purpose aircraft simulator cockpit of Cessna
CN114638442A (en) * 2022-05-19 2022-06-17 珠海翔翼航空技术有限公司 Flight training scheme generation system, method and equipment for individual difference
CN115314692A (en) * 2022-10-12 2022-11-08 珠海翔翼航空技术有限公司 Image communication method and device
CN116524781A (en) * 2023-07-03 2023-08-01 中国科学院长春光学精密机械与物理研究所 Simulation training and evaluating method and system for photoelectric measurement and control equipment

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6077077A (en) * 1997-05-22 2000-06-20 American Airlines Architecture and process for simulating the data transmitted to a navigation management computer
US20020187460A1 (en) * 2001-06-08 2002-12-12 Eurocopter Deutschland Gmbh Method and device for reproducing a recorded flight mission of an aircraft from an observer position by means of a system for flight simulation
CN101714302A (en) * 2009-12-15 2010-05-26 中国民航大学 Automatic-piloting simulator of aeroplane
CN201698611U (en) * 2010-06-30 2011-01-05 郭蓉晖 Virtual simulation flight simulator
CN102053563A (en) * 2010-12-27 2011-05-11 刘宇 Flight training data acquisition and quality evaluation system of analog machine
CN202217408U (en) * 2011-07-08 2012-05-09 中国民航科学技术研究院 Flight training device
CN103136979A (en) * 2011-11-29 2013-06-05 中国商用飞机有限责任公司 Airplane comprehensive procedural training device and throttle lever device
CN203366575U (en) * 2012-11-27 2013-12-25 中国民用航空飞行学院 Flight training device for diminutive aeroplane

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6077077A (en) * 1997-05-22 2000-06-20 American Airlines Architecture and process for simulating the data transmitted to a navigation management computer
US20020187460A1 (en) * 2001-06-08 2002-12-12 Eurocopter Deutschland Gmbh Method and device for reproducing a recorded flight mission of an aircraft from an observer position by means of a system for flight simulation
CN101714302A (en) * 2009-12-15 2010-05-26 中国民航大学 Automatic-piloting simulator of aeroplane
CN201698611U (en) * 2010-06-30 2011-01-05 郭蓉晖 Virtual simulation flight simulator
CN102053563A (en) * 2010-12-27 2011-05-11 刘宇 Flight training data acquisition and quality evaluation system of analog machine
CN202217408U (en) * 2011-07-08 2012-05-09 中国民航科学技术研究院 Flight training device
CN103136979A (en) * 2011-11-29 2013-06-05 中国商用飞机有限责任公司 Airplane comprehensive procedural training device and throttle lever device
CN203366575U (en) * 2012-11-27 2013-12-25 中国民用航空飞行学院 Flight training device for diminutive aeroplane

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104809935A (en) * 2015-05-13 2015-07-29 中国航空工业集团公司沈阳飞机设计研究所 Simulation training method for special situation fault of unmanned aerial vehicle and system thereof
WO2017107323A1 (en) * 2015-12-22 2017-06-29 成都艾尔伯特科技有限责任公司 Flight simulation entertainment experience apparatus
CN107067873A (en) * 2016-11-25 2017-08-18 上海航空电器有限公司 The flight simulation flight Horizon table controlled based on CAN
CN107067873B (en) * 2016-11-25 2022-03-29 上海航空电器有限公司 Aviation simulation flight horizon table based on CAN bus control
CN109062629A (en) * 2018-07-13 2018-12-21 成都泛美视界科技有限公司 A kind of performance optimization method of flight simulation software
CN109243243A (en) * 2018-10-08 2019-01-18 卓尔飞机制造(武汉)有限公司 Flight simulation simulation training system and its Training Methodology
CN109243243B (en) * 2018-10-08 2020-12-04 卓尔飞机制造(武汉)有限公司 Flight simulation training system and training method thereof
CN110164236A (en) * 2019-05-28 2019-08-23 四川信息职业技术学院(广元无线电技工学校) Multi-functional unmanned plane teaching test case
CN110335519A (en) * 2019-07-16 2019-10-15 上海卡索航空科技有限公司 A kind of 172 general-purpose aircraft simulator cockpit of Cessna
CN114638442A (en) * 2022-05-19 2022-06-17 珠海翔翼航空技术有限公司 Flight training scheme generation system, method and equipment for individual difference
CN115314692A (en) * 2022-10-12 2022-11-08 珠海翔翼航空技术有限公司 Image communication method and device
CN116524781A (en) * 2023-07-03 2023-08-01 中国科学院长春光学精密机械与物理研究所 Simulation training and evaluating method and system for photoelectric measurement and control equipment

Similar Documents

Publication Publication Date Title
CN104064071A (en) Small fixed flight training device system
CN111195433B (en) Virtual reality with virtualization in trainer and test environments
KR101552561B1 (en) A configurable simulator for performing a distributed simulation
CN104050332A (en) Distributed-type real-time comprehensive simulation method of avionics system
CN102566441A (en) Visual simulation test system for unmanned aerial vehicle (UAV)
KR101552560B1 (en) A configurable simulator with a plurality of configurable modular cards
CN102902517A (en) Method of emulating a controller pilot data link communication human machine interface
US20150111180A1 (en) Methods, systems, and computer readable media for cursor and text entry for aircraft interface simulation
CA2850540A1 (en) Portable device to manage and control an air traffic control training system
CN109920300A (en) A kind of military fighter aircraft driving simulation system
CN110187681A (en) Restructural cockpit display & control system
CN106781928B (en) Virtual-real combined crane electric control simulation system
CN106773789B (en) Operation and display system of engineering simulator
CN104503259A (en) Universal programmable aircraft simulator system for launch control system
CN103942384A (en) Dynamic aircraft assembly scene real-time and three-dimensional visualization method based on head-mounted displayer
CN107886800A (en) A kind of aircraft cockpit avionics simulation system of people in the loop
CN201698611U (en) Virtual simulation flight simulator
CN110027718B (en) Touch display control system for large civil aircraft cockpit
CN204965047U (en) Embedded synthesis shows emulation instrument based on ARM
CN203727651U (en) Display control system applied to fighter
CN202217408U (en) Flight training device
CN206058607U (en) The airborne multiple functional displayss of HWIL simulation
CN206147979U (en) Comprehensive test simulation training system
KR20200099229A (en) Avionics simulation system and method
CN205862130U (en) HWIL simulation cockpit display & control system

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
RJ01 Rejection of invention patent application after publication
RJ01 Rejection of invention patent application after publication

Application publication date: 20140924