CN104269083A - Low-cost flight simulator cabin display and control system - Google Patents
Low-cost flight simulator cabin display and control system Download PDFInfo
- Publication number
- CN104269083A CN104269083A CN201410462404.2A CN201410462404A CN104269083A CN 104269083 A CN104269083 A CN 104269083A CN 201410462404 A CN201410462404 A CN 201410462404A CN 104269083 A CN104269083 A CN 104269083A
- Authority
- CN
- China
- Prior art keywords
- control
- display
- instrument
- control system
- cabin
- 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
Links
Classifications
-
- G—PHYSICS
- G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
- G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
- G09B9/00—Simulators for teaching or training purposes
- G09B9/02—Simulators for teaching or training purposes for teaching control of vehicles or other craft
- G09B9/08—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer
Abstract
The invention discloses a low-cost flight simulator cabin display and control system which is a combined training simulator cabin display and control system used for large aircraft air-service and ground-service personal training. The low-cost flight simulator cabin display and control system is an interface for transmitting information between an operator and a flight simulator, is composed of a display part and a control part and is composed of a simulated cabin, control mechanisms, a resolving control computer, an instrument emulation computer, displayers and control templates. The displayers display instruments and various control signals, the control templates with integrated control knobs and switches are installed outside the displayers for achieving man-machine interaction, the control templates and the displayers are assembled according to the proportions of a true aircraft, and the simulated cabin is built. According to the low-cost flight simulator cabin display and control system, the method that the virtual instruments and the control templates are combined is used; compared with a full-hardware simulator based on solid instruments, the device structure of the simulator is simplified, the development cost is reduced, the development cycle is shortened, and the design change efficiency of the system is improved; meanwhile, the problem that the man-machine interaction fidelity of a virtual display and control system based on the touch technology is not high can be solved.
Description
Technical field
The present invention relates to the synthetic Simulator the cockpit display and control system that a kind of, ground crew empty for large aircraft used on ground trains, be the interface of transmission of information between manipulation personnel and flight simulator, form by showing and controlling two parts.
Background technology
Utilize flight simulator to carry out flight training, have the initiative of saving training cost, improving training effectiveness, guarantee flight safety, improving training and ageing, reduce the plurality of advantages such as environmental pollution.Therefore, in modern flight training process, a large amount of employs flight simulator as auxiliary training tool, requires that flight simulator has higher fidelity.Flight simulator passenger cabin display & control system comprises display and controls two parts, and display section is the interface that pilot obtains information, mainly shows the various information such as aircraft altitude, speed, boat appearance, course and engine behavior; And control is the interface of manipulation personnel issuing command, the change of the state parameters such as maneuvering device, gauge tap, knob, button, instrument and pilot lamp also respective change.Passenger cabin display & control system can create the same cabin ambient of a kind of and true aircraft for manipulation personnel on sense organ, thus match with vision emulation system and simulate real flight environment of vehicle, it is the platform that manipulation personnel and flight simulator information are transmitted, and is core and the basis of virtual reality emulation.Therefore, in the design process of large aircraft simulator, the design of Simulation of passenger cabin display & control system directly has influence on the performance index of flight simulator.
At present, passenger cabin display & control system emulation mode mainly contains devices at full hardware emulation and the virtual emulation based on touch technology.Devices at full hardware emulation refers to builds passenger cabin display & control system with Instrumentation and Control panel in kind, instrument in kind is self-contained, namely itself is with the ability of input and output, instrument there are the functions such as button, knob, scale, figure, include digital-to-analogue, analog to digital converter, microprocessor, storer, bus etc. in gauge internal, all circuit are all fixing.Advantage is: display effect is true to nature, man-machine interaction is friendly, shortcoming is: due to Flight Instrument One's name is legion, broad categories, be that repacking finished product instrument or designed, designed exploitation all need high expense, the expense building devices at full hardware passenger cabin display & control system can account for more than 40% of overall R & D Cost; Instrument control mode in simulator is different from true instrument with logical relation, needs to redesign dial plate and inner drive connection, and the construction cycle is long; Gauge internal complex structure in kind, the degree of modularity is not high, causes that troubleshooting difficulty is large, maintenance cost is high; Instrument function in kind is fixed, restricted with the connection of other equipment, and information is difficult to conversion, and upgradability is weak.Virtual display & control system based on touch technology is a kind of pure virtual passenger cabin display & control system, graphical simulation technology and the 3D technology of application component-oriented generate the virtual instrument picture with 3D vision effect, shown by display, install touch-screen over the display additional and realize man-machine interaction.Virtual instrument is then core with computing machine, makes full use of the powerful display of computing machine, processing procedure that process, storage capacity carry out analog physical instrument.The function that various " control " on virtual instrument panel completes with various " parts " on conventional instrument panel is identical, and user, by touch-screen input control order, shows corresponding effect by resolving the rear instrument of process.Advantage is: intuitive display, with low cost, upgrades upgrading convenient.Shortcoming is: virtual display & control system realizes man-machine interaction by touch-screen, cannot analog band insurance or error protection gauge tap, knob real operational processes, can not give the real interactive feel of manipulation personnel, simulation fidelity is not high, and feeling of immersion is not strong; The needs that touch-screen control accuracy and sensitivity quick and precisely operate when cannot meet managing special situation, when carrying out multi-mode operation, multi-point touch is easily disturbed especially simultaneously, causes operating process mistake, and evaluation result can not reflect manipulation personnel flight level really.
Summary of the invention
The present invention is that a kind of cost is low, precision is high, good reliability, be convenient to safeguard, flight simulator passenger cabin display & control system easy to use, just other type can be changed over by upgrade software and Control architecture, be with good expansibility, overcome the deficiency that existing flight simulator passenger cabin display & control system emulation mode exists.
Technical scheme of the present invention is about a kind of low cost flight simulator passenger cabin display & control system: comprise the control wheel in passenger cabin, pedal, control stand and instrument display control device, wherein said control wheel, pedal and control stand adopt matter emulation, instrument display control device is by several instrument displays and integrated electric switch, the Control architecture composition of knob, this device also comprises instrument simulation computing machine and interface system, split screen display card, display Displaying Meter and all kinds of control signal, at instrument display, integrating control knob is installed outward, the Control architecture of electric switch realizes the input of steering order, resolve computer for controlling and gather control wheel by bus, pedal, throttle, knob, the control signal of electric switch sends to instrument simulation computing machine, by driver, instrument is controlled in real time, Control architecture and display assemble according to the ratio of true aircraft, build analog capsule cabin, GL Studio software development technique is used in the three-dimensional modeling and emulation of instrument.
A kind of low cost flight simulator passenger cabin display & control system, Control architecture adopts aluminium sheet to process according to instrument panel physical size, position, the shape of instrument are corresponding with display display section, on Control architecture, installation kit is containing the meter case model of button, knob, and Control architecture and true passenger cabin are consistent.
Effect of the present invention is: utilize display and Control architecture to replace devices at full hardware display & control system to reduce the design and manufacture cost of system, reduce the R&D cycle; This passenger cabin display & control system utilizes Control architecture to send control signal to main control computer, then control information is sent to virtual instrument display by main control computer, this kind of interactive mode virtual display & control system that can solve based on touch technology touches that precision is not high, multi-point touch be easily disturbed cause operating process mistake, can not analog band insurance or error protection gauge tap, knob the problem of real operational processes; Just display & control system can be upgraded to other type by amendment software and structural control template, adapt to higher mission requirements, therefore, extensibility and the reusability of system are strong; Whole system is by software control, and compared with devices at full hardware display & control system, do not have complicated equipment composition, system works long hours less to hardware deterioration, good reliability, and working service is convenient.
Accompanying drawing explanation
Fig. 1 is passenger cabin display & control system integral layout.
Fig. 2 passenger cabin display & control system hardware structure diagram.
Fig. 3 is monolithic aobvious control unit virtual instrument layout.
Fig. 4 is monolithic aobvious control unit controls template layout.
Fig. 5 is monolithic aobvious control unit assembling schematic diagram.
Fig. 6 is virtual instrument modeling process figure.
Fig. 7 virtual instrument system process flow diagram.
In figure: (1) is Left-Hand Drive panel; (2) be front panel (left side); (3) be central control panel; (4) for front panel (in); (5) be front panel (right side); (6) be right side control panel; (7) be Right-Hand Side Console; (8) be right pedal; (9) be right control wheel; (10) be center pedestal; (11) be left-hand drive dish; (12) for left foot is pedaled; (13) be Left-Hand Side Console.
Embodiment
The specific embodiment of the present invention is: the flight simulator passenger cabin display & control system building a kind of low cost, as shown in Figure 1, comprise Left-Hand Drive panel (1), front panel (left side) (2), central control panel (3), front panel (in) (4), front panel (right side) (5), right side control panel (6), Right-Hand Side Console (7), right pedal (8), right control wheel (9), center pedestal (10), left-hand drive dish (11), left foot pedal (12), Left-Hand Side Console (13).Wherein, front panel (left side) (2), central control panel (3), front panel (right side) (5) are the interfaces that aircrew manipulates, and mainly show the information such as aspect, flying height, speed, orientation; Left-Hand Drive panel (1), front panel (in) (4) be aircraft observer,flight engineer's operation and control interface, each systematic parameter of main display engine; Right side control panel (6) is aerial electrically teacher's operation and control interface, main display aircraft electrical power supply system parameter.These six interfaces are main interfaces of passenger cabin display & control system, and display contains much information, and manipulation is frequent, and the emulation mode adopting virtual instrument to add Control architecture builds, and reduces costs.Right-Hand Side Console (7), left control stand (13) mainly comprise control electric switch, knob and button, therefore only need to make the emulation that Control architecture can realize operation and control interface.The catanator that right pedal (8), right control wheel (9), left-hand drive dish (11), left foot pedal (12), center pedestal (10) is aircrew's transmitting control information, be connected with sensor, control information is passed to main control computer resolve, fed back by various instrument, each control gear processes according to interior of aircraft physical size.Main control computer and virtual instrument computing machine are arranged in the body of cabin, main control computer is connected with all sensors in passenger cabin by interface system, receiving sensor data, pass to virtual instrument computing machine, virtual instrument computing machine is connected with corresponding display interface by split screen display card, and the flight parameter received is shown to each interface.
Passenger cabin display & control system hardware configuration as shown in Figure 2, instrument simulation computing machine (1) drives three pieces, front panel left, center, right display by split screen display card, mainly shows aspect, flying height, speed, orientation, engine major parameter and all kinds of alarm signal; Instrument simulation computing machine (2) drives Left-Hand Drive panel display, right side control panel display and central control panel display three pieces of displays by split screen display card, main display aircraft electrical power supply system parameter, each subsystem parameter of engine, communication and navigation systematic parameter.Six pieces of Control architecture are assembled together with corresponding six pieces of displays by erecting frame, the electric switch of Control architecture, knob, button are mainly produced all kinds of control signal and are transferred to by CAN and resolve computer for controlling, realize dispersion Real-time Collection, control centralized management, information resources share.Left control stand (13), right control stand (7), center pedestal (10) and catanator (8,9,11,12) pass through Object copying, main generation control signal and feedback signal, by CAN with resolve computer for controlling real-time communication.Resolve computer for controlling and receive digital quantity and analog quantity 2 class input signal, wherein digital quantity input is produced by on-off model such as electric switch, switch, buttons, and analog input is mainly produced by simulating signals such as control wheel, pedal, throttle control handle, knobs; Feedback signal is digital quantity signal, and the control signal of electric switch, button is mainly fed back to the signal lamp on Control architecture by feedback signal.Resolve after input signal is resolved by Ethernet by computer for controlling and send instrument simulation computing machine to, the control information of input is published to each instrument by instrument simulation computing machine, by split screen display card, three-dimensional picture is real-time transmitted to each display.
Monolithic aobvious control unit comprises simulation computer, split screen display card, display and Control architecture.Simulation computer adopts reinforced general purpose PC to complete generation and the driving of figure, is completed the display of instrument picture by split screen display card driving display.Display driver card need be supported 1920 × 1080 pixels, triple channel independent drawing driver output, have the adjustable ginseng split screen display driver card of full screen antialiasing and the anti-aliasing function of full screen, can reduce the quantity of simulation computer like this, cost-saving.For realizing the integral layout of passenger cabin display & control system, guarantee overall visual effect in cabin and do not affect the manipulation of operating personnel, choosing of display overall dimensions controls in Control architecture coverage, ensures display and the position coordination between Control architecture and installing frame.For left panel, display selects 42 cun of LED liquid crystal display, is fixed on by display in erecting frame, and virtual instrument display layout is consistent with actual ratio, as shown in Figure 3.Control architecture adopts aluminium sheet to process according to instrument panel physical size, position, the shape of instrument are corresponding with display display section, on Control architecture, installation kit is containing the meter case model of button, knob, the interactive feel of Control architecture and true passenger cabin are consistent, and Control architecture layout (for left panel) as shown in Figure 4.Display and Control architecture adopt bolts assemblies, and assembling schematic diagram as shown in Figure 5.Due to Control architecture and display assemble after distance narrow and small, meter case model and display section are basic to be used up the instrument panel scope of blocking, be exposed to beyond the scope of blocking to not make signal cable, controller line plate adopts centralized layout, divide two layers of layout, in limited usage space, obtain feasible layout.
The design of virtual instrument software, except realizing the basic function of system, also will consider the reliability of system cloud gray model, stability, high efficiency and real-time.Virtual instrument software have employed Target-oriented thought in the design process, GL Studio is utilized to complete the modeling of virtual instrument, concrete modeling process is as shown in Figure 6: 1. create instrument texture, namely adopts image processing software to produce the picture of required texture, as dial plate texture and indicator texture etc.; 2. according to the display requirement of instrument, create polygon and stick texture, figure is renamed, specifying call back function and behavior etc.; 3. instrument is created instrument cluster, be convenient to reuse; 4. add code in the application, for instrument creates behavior, call control function, as rotation, movement, convergent-divergent etc., complete the Dynamic controlling to object; 5. the behavior code write and graph data are converted into C++ class code; 6. on VC++ platform, carry out compile and test, check display effect, if dissatisfied, get back to second step.Utilize Visual C++ programmed environment to complete data communication and the instrument drive of virtual instrument, program mainly comprises that Ethernet data receives, data resolve, create the functional module such as sharing data area and instrument drive, and Fig. 7 is virtual instrument system process flow diagram.Because instrument drive equation solver is complicated, also want to carry out multichannel real-time communication with other system simultaneously, for ensureing the reliable and stable work of system, adopt multithread programming method in the design process, instrument drive, instrument three-dimensional model and data communication is encapsulated respectively by independent class, effectively utilize computer resource, be also convenient to carry out Function Extension and system maintenance.In data communication, resolve computer for controlling and use 100M/1000M self-adaptation Ethernet, with broadcast mode unidirectional delivery data to instrument simulation computing machine, data reception module opens up data buffer area in instrument simulation computing machine, deposits the Ethernet broadcast data received.Virtual instrument driver module finds out array corresponding with it by the demand of passage from the broadcast data buffer area received, carry out data by Logic judgment, Nonlinear Processing to resolve, data through resolving stored in shared drive data field, thus complete the display driver to meter control with shared drive data layout.
Claims (1)
1. a low cost flight simulator passenger cabin display & control system, comprise the control wheel in passenger cabin, pedal, control stand and instrument display control device, wherein control wheel, pedal and control stand adopt matter emulation, instrument display control device is by several instrument displays and integrated electric switch, the Control architecture composition of knob, this device also comprises instrument simulation computing machine and interface system, split screen display card, display Displaying Meter and all kinds of control signal, at instrument display, integrating control knob is installed outward, the Control architecture of electric switch realizes the input of steering order, resolve computer for controlling and gather control wheel by bus, pedal, throttle, knob, the control signal of electric switch sends to instrument simulation computing machine, by driver, instrument is controlled in real time, Control architecture and display assemble according to the ratio of true aircraft, build analog capsule cabin, GL Studio software development technique is used in the three-dimensional modeling and emulation of instrument.
It is characterized in that: Control architecture adopts aluminium sheet to process according to instrument panel physical size, position, the shape of instrument are corresponding with display display section, on Control architecture, installation kit is containing the meter case model of button, knob, and Control architecture and true passenger cabin are consistent.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410462404.2A CN104269083A (en) | 2014-09-04 | 2014-09-04 | Low-cost flight simulator cabin display and control system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410462404.2A CN104269083A (en) | 2014-09-04 | 2014-09-04 | Low-cost flight simulator cabin display and control system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104269083A true CN104269083A (en) | 2015-01-07 |
Family
ID=52160600
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410462404.2A Pending CN104269083A (en) | 2014-09-04 | 2014-09-04 | Low-cost flight simulator cabin display and control system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104269083A (en) |
Cited By (23)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104765280A (en) * | 2015-03-13 | 2015-07-08 | 吉林医药学院 | Unmanned aerial vehicle three-dimensional display control comprehensive-training system |
| WO2016154706A1 (en) * | 2015-03-31 | 2016-10-06 | Cae Inc. | Modular infrastructure for an interactive computer program |
| WO2016154707A1 (en) * | 2015-03-31 | 2016-10-06 | Cae Inc. | Interactive computer program with virtualized participant |
| US9473767B1 (en) | 2015-03-31 | 2016-10-18 | Cae Inc. | Multifactor eye position identification in a display system |
| CN106128210A (en) * | 2016-08-18 | 2016-11-16 | 信阳泰蓝仿真科技有限公司 | A kind of airborne radar Repair Training System and control method thereof |
| CN106648519A (en) * | 2015-10-28 | 2017-05-10 | 大陆汽车电子(芜湖)有限公司 | Method for detecting actual display effect of picture for instrument |
| US9754506B2 (en) | 2015-03-31 | 2017-09-05 | Cae Inc. | Interactive computer program with virtualized participant |
| CN107464471A (en) * | 2017-08-09 | 2017-12-12 | 上海工程技术大学 | A kind of display system and control method for flight simulator |
| 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 |
| CN108109471A (en) * | 2016-11-24 | 2018-06-01 | 上海航空电器有限公司 | Flight simulation flying height table based on CAN bus control |
| CN108281060A (en) * | 2018-04-04 | 2018-07-13 | 北京瀚科瑞杰科技发展有限公司 | A kind of emulation cockpit panel module for flight simulation |
| CN108648558A (en) * | 2018-06-22 | 2018-10-12 | 中国人民解放军国防科技大学 | Manned and unmanned aerial vehicle collaborative drilling simulation cabin |
| CN109163192A (en) * | 2018-11-19 | 2019-01-08 | 中国航空综合技术研究所 | Combined display based on flexible analog capsule cabin adjusts and positioning device |
| CN109987253A (en) * | 2019-04-17 | 2019-07-09 | 上海卡索航空科技有限公司 | A kind of aircraft cockpit instrument 2D the Realization of Simulation system |
| CN110444077A (en) * | 2019-08-26 | 2019-11-12 | 中仿智能科技（上海）股份有限公司 | A kind of Virtual Cockpit System of simulated flight device |
| CN110992770A (en) * | 2020-01-06 | 2020-04-10 | 中仿智能科技（上海）股份有限公司 | Flight simulator system |
| CN111047946A (en) * | 2020-01-14 | 2020-04-21 | 中仿智能科技（上海）股份有限公司 | Full-function flight simulator |
| US10649580B1 (en) | 2011-08-05 | 2020-05-12 | P4tents1, LLC | Devices, methods, and graphical use interfaces for manipulating user interface objects with visual and/or haptic feedback |
| CN111754836A (en) * | 2020-07-23 | 2020-10-09 | 北京道迩科技有限公司 | Simulation training system |
| CN113706969A (en) * | 2021-08-23 | 2021-11-26 | 天津津航计算技术研究所 | Virtual-real combined helicopter cabin system |
| CN114141095A (en) * | 2021-11-22 | 2022-03-04 | 芜湖航翼集成设备有限公司 | Flight simulator semi-physical simulation instrument system and implementation method thereof |
| US11294458B2 (en) | 2015-03-31 | 2022-04-05 | Cae Inc. | Modular infrastructure for an interactive computer program |
| CN115359696A (en) * | 2022-07-18 | 2022-11-18 | 上海卡索航空科技有限公司 | Single-seat fighter combat environment simulation equipment |
Citations (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4599070A (en) * | 1981-07-29 | 1986-07-08 | Control Interface Company Limited | Aircraft simulator and simulated control system therefor |
| JPH08286600A (en) * | 1995-04-11 | 1996-11-01 | Mitsubishi Heavy Ind Ltd | Airplane design simulator |
| US5616030A (en) * | 1994-06-01 | 1997-04-01 | Watson; Bruce L. | Flight simulator employing an actual aircraft |
| US20030023740A1 (en) * | 2001-02-17 | 2003-01-30 | White Daryl A. | System and method for operating software in a flight simulator environment |
| US20060160049A1 (en) * | 2005-01-14 | 2006-07-20 | Faiek Zora | Flight simulator panel with active graphic display instrumentation |
| CN101251959A (en) * | 2008-02-04 | 2008-08-27 | 于辉 | General-purpose aviation simulator based on virtual operation |
| CN201242814Y (en) * | 2008-07-01 | 2009-05-20 | 中国人民解放军空军第一航空学院 | Single-cargo single-seat airplane synthesis safeguard simulation training system control device |
| CN102013187A (en) * | 2010-10-29 | 2011-04-13 | 北京航空航天大学 | Flight simulator system with persistent overload simulation capability |
| CN102053563A (en) * | 2010-12-27 | 2011-05-11 | 刘宇 | Flight training data acquisition and quality evaluation system of analog machine |
| CN102087675A (en) * | 2010-06-29 | 2011-06-08 | 北京航空航天大学 | Flight simulation system with design and test functions of information display interface |
| CN203366575U (en) * | 2012-11-27 | 2013-12-25 | 中国民用航空飞行学院 | Flight training device for diminutive aeroplane |
| CN103473966A (en) * | 2013-08-29 | 2013-12-25 | 南京航空航天大学 | Semi-physical digital simulation control platform of aircraft cockpit |
| CN103760780A (en) * | 2014-02-17 | 2014-04-30 | 中国航空无线电电子研究所 | Universal simulation platform of cockpit display control system |
-
2014
- 2014-09-04 CN CN201410462404.2A patent/CN104269083A/en active Pending
Patent Citations (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4599070A (en) * | 1981-07-29 | 1986-07-08 | Control Interface Company Limited | Aircraft simulator and simulated control system therefor |
| US5616030A (en) * | 1994-06-01 | 1997-04-01 | Watson; Bruce L. | Flight simulator employing an actual aircraft |
| JPH08286600A (en) * | 1995-04-11 | 1996-11-01 | Mitsubishi Heavy Ind Ltd | Airplane design simulator |
| US20030023740A1 (en) * | 2001-02-17 | 2003-01-30 | White Daryl A. | System and method for operating software in a flight simulator environment |
| US20060160049A1 (en) * | 2005-01-14 | 2006-07-20 | Faiek Zora | Flight simulator panel with active graphic display instrumentation |
| CN101251959A (en) * | 2008-02-04 | 2008-08-27 | 于辉 | General-purpose aviation simulator based on virtual operation |
| CN201242814Y (en) * | 2008-07-01 | 2009-05-20 | 中国人民解放军空军第一航空学院 | Single-cargo single-seat airplane synthesis safeguard simulation training system control device |
| CN102087675A (en) * | 2010-06-29 | 2011-06-08 | 北京航空航天大学 | Flight simulation system with design and test functions of information display interface |
| CN102013187A (en) * | 2010-10-29 | 2011-04-13 | 北京航空航天大学 | Flight simulator system with persistent overload simulation capability |
| CN102053563A (en) * | 2010-12-27 | 2011-05-11 | 刘宇 | Flight training data acquisition and quality evaluation system of analog machine |
| CN203366575U (en) * | 2012-11-27 | 2013-12-25 | 中国民用航空飞行学院 | Flight training device for diminutive aeroplane |
| CN103473966A (en) * | 2013-08-29 | 2013-12-25 | 南京航空航天大学 | Semi-physical digital simulation control platform of aircraft cockpit |
| CN103760780A (en) * | 2014-02-17 | 2014-04-30 | 中国航空无线电电子研究所 | Universal simulation platform of cockpit display control system |
Non-Patent Citations (3)
| Title |
|---|
| 孙鑫等: "基于RS-485总线的飞行模拟器座舱仪表控制", 《青岛大学学报（工程技术版）》 * |
| 徐强等: "飞行模拟器座舱仪表通信技术研究", 《信息技术》 * |
| 王述运等: "基于CAN总线的飞行模拟器座舱系统设计", 《软件》 * |
Cited By (35)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US10996787B1 (en) | 2011-08-05 | 2021-05-04 | P4tents1, LLC | Gesture-equipped touch screen system, method, and computer program product |
| US11061503B1 (en) | 2011-08-05 | 2021-07-13 | P4tents1, LLC | Devices, methods, and graphical user interfaces for manipulating user interface objects with visual and/or haptic feedback |
| US10656759B1 (en) | 2011-08-05 | 2020-05-19 | P4tents1, LLC | Devices, methods, and graphical user interfaces for manipulating user interface objects with visual and/or haptic feedback |
| US10649580B1 (en) | 2011-08-05 | 2020-05-12 | P4tents1, LLC | Devices, methods, and graphical use interfaces for manipulating user interface objects with visual and/or haptic feedback |
| US10788931B1 (en) | 2011-08-05 | 2020-09-29 | P4tents1, LLC | Devices, methods, and graphical user interfaces for manipulating user interface objects with visual and/or haptic feedback |
| US11740727B1 (en) | 2011-08-05 | 2023-08-29 | P4Tents1 Llc | Devices, methods, and graphical user interfaces for manipulating user interface objects with visual and/or haptic feedback |
| US10649581B1 (en) | 2011-08-05 | 2020-05-12 | P4tents1, LLC | Devices, methods, and graphical user interfaces for manipulating user interface objects with visual and/or haptic feedback |
| US10671213B1 (en) | 2011-08-05 | 2020-06-02 | P4tents1, LLC | Devices, methods, and graphical user interfaces for manipulating user interface objects with visual and/or haptic feedback |
| CN104765280A (en) * | 2015-03-13 | 2015-07-08 | 吉林医药学院 | Unmanned aerial vehicle three-dimensional display control comprehensive-training system |
| US9754506B2 (en) | 2015-03-31 | 2017-09-05 | Cae Inc. | Interactive computer program with virtualized participant |
| WO2016154706A1 (en) * | 2015-03-31 | 2016-10-06 | Cae Inc. | Modular infrastructure for an interactive computer program |
| US11294458B2 (en) | 2015-03-31 | 2022-04-05 | Cae Inc. | Modular infrastructure for an interactive computer program |
| WO2016154707A1 (en) * | 2015-03-31 | 2016-10-06 | Cae Inc. | Interactive computer program with virtualized participant |
| US9473767B1 (en) | 2015-03-31 | 2016-10-18 | Cae Inc. | Multifactor eye position identification in a display system |
| CN106648519A (en) * | 2015-10-28 | 2017-05-10 | 大陆汽车电子(芜湖)有限公司 | Method for detecting actual display effect of picture for instrument |
| CN106648519B (en) * | 2015-10-28 | 2020-02-18 | 大陆汽车车身电子系统（芜湖）有限公司 | Method for detecting actual display effect of picture for instrument |
| CN106128210B (en) * | 2016-08-18 | 2019-04-12 | 信阳泰蓝仿真科技有限公司 | A kind of airborne radar Repair Training System and its control method |
| CN106128210A (en) * | 2016-08-18 | 2016-11-16 | 信阳泰蓝仿真科技有限公司 | A kind of airborne radar Repair Training System and control method thereof |
| CN108109471A (en) * | 2016-11-24 | 2018-06-01 | 上海航空电器有限公司 | Flight simulation flying height table based on CAN bus control |
| CN107464471B (en) * | 2017-08-09 | 2019-09-10 | 上海工程技术大学 | A kind of display system and control method for flight simulator |
| CN107464471A (en) * | 2017-08-09 | 2017-12-12 | 上海工程技术大学 | A kind of display system and control method for flight simulator |
| 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 |
| CN108281060B (en) * | 2018-04-04 | 2024-02-09 | 北京瀚科科技集团有限公司 | A emulation cabin panel module for flight simulation |
| CN108281060A (en) * | 2018-04-04 | 2018-07-13 | 北京瀚科瑞杰科技发展有限公司 | A kind of emulation cockpit panel module for flight simulation |
| CN108648558B (en) * | 2018-06-22 | 2020-06-26 | 中国人民解放军国防科技大学 | Manned and unmanned aerial vehicle collaborative drilling simulation cabin |
| CN108648558A (en) * | 2018-06-22 | 2018-10-12 | 中国人民解放军国防科技大学 | Manned and unmanned aerial vehicle collaborative drilling simulation cabin |
| CN109163192A (en) * | 2018-11-19 | 2019-01-08 | 中国航空综合技术研究所 | Combined display based on flexible analog capsule cabin adjusts and positioning device |
| CN109987253A (en) * | 2019-04-17 | 2019-07-09 | 上海卡索航空科技有限公司 | A kind of aircraft cockpit instrument 2D the Realization of Simulation system |
| CN110444077A (en) * | 2019-08-26 | 2019-11-12 | 中仿智能科技（上海）股份有限公司 | A kind of Virtual Cockpit System of simulated flight device |
| CN110992770A (en) * | 2020-01-06 | 2020-04-10 | 中仿智能科技（上海）股份有限公司 | Flight simulator system |
| CN111047946A (en) * | 2020-01-14 | 2020-04-21 | 中仿智能科技（上海）股份有限公司 | Full-function flight simulator |
| CN111754836A (en) * | 2020-07-23 | 2020-10-09 | 北京道迩科技有限公司 | Simulation training system |
| CN113706969A (en) * | 2021-08-23 | 2021-11-26 | 天津津航计算技术研究所 | Virtual-real combined helicopter cabin system |
| CN114141095A (en) * | 2021-11-22 | 2022-03-04 | 芜湖航翼集成设备有限公司 | Flight simulator semi-physical simulation instrument system and implementation method thereof |
| CN115359696A (en) * | 2022-07-18 | 2022-11-18 | 上海卡索航空科技有限公司 | Single-seat fighter combat environment simulation equipment |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN104269083A (en) | Low-cost flight simulator cabin display and control system | |
| CN101251959B (en) | General-purpose aviation simulator based on virtual operation | |
| EP0872819B1 (en) | Training simulators | |
| CN100568317C (en) | Control apparatus for airplane synthetic guarantee simulated training system | |
| CN203366575U (en) | Flight training device for diminutive aeroplane | |
| CN103473966A (en) | Semi-physical digital simulation control platform of aircraft cockpit | |
| CN201242814Y (en) | Single-cargo single-seat airplane synthesis safeguard simulation training system control device | |
| CN102663921A (en) | Multi-channel and multi-screen three dimensional immersion simulation system of ship steering and operation | |
| CN103065022A (en) | Incentive model simulation platform for aerocraft electronic system | |
| US20150111180A1 (en) | Methods, systems, and computer readable media for cursor and text entry for aircraft interface simulation | |
| CN113496635B (en) | Flight simulator and flight training simulation method | |
| CN111047946A (en) | Full-function flight simulator | |
| CN105116756A (en) | ARM based embedded integrated display simulation instrument | |
| CN110246389A (en) | A kind of ladder vehicle training system and method | |
| CN102324196A (en) | Simulation training and evaluation semi-physical simulation system of aviation hydraulic oil pump vehicle | |
| CN106781928A (en) | The crane electronic control simulation system that a kind of actual situation is combined | |
| Ackerman et al. | Pilot-in-the-loop flight simulator for NASA’s Transport Class Model | |
| CN202757953U (en) | Tester for automobile instrument | |
| CN115145167A (en) | Civil aircraft cockpit design iteration simulation system | |
| CN204965047U (en) | Embedded synthesis shows emulation instrument based on ARM | |
| CN104281448B (en) | A kind of combined type vision emulation system for supporting that function is customized and emulation mode | |
| CN109323878B (en) | Flight simulator hardware detection system based on WPF | |
| RU108685U1 (en) | UNIVERSAL PILOT MODELING STAND | |
| RU124965U1 (en) | VIDEO INFORMATION FORMING DEVICE FOR AIRCRAFT ELECTRONIC INDICATION SYSTEM | |
| CN212484650U (en) | Panel of airplane simulator |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20150107 |