CN103473966A - Semi-physical digital simulation control platform of aircraft cockpit - Google Patents
Semi-physical digital simulation control platform of aircraft cockpit Download PDFInfo
- Publication number
- CN103473966A CN103473966A CN2013103836699A CN201310383669A CN103473966A CN 103473966 A CN103473966 A CN 103473966A CN 2013103836699 A CN2013103836699 A CN 2013103836699A CN 201310383669 A CN201310383669 A CN 201310383669A CN 103473966 A CN103473966 A CN 103473966A
- Authority
- CN
- China
- Prior art keywords
- data
- instrument
- aircraft
- simulation
- show
- 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
Landscapes
- Management, Administration, Business Operations System, And Electronic Commerce (AREA)
- Processing Or Creating Images (AREA)
Abstract
The invention discloses a semi-physical digital simulation control platform of an aircraft cockpit, belonging to the technical field of aircraft simulation control. The digital simulation control platform comprises a cockpit vision system, a flight control device, a data acquisition system, a display device which is arranged in a simulation cockpit and a central control board and used for real-time display of data of instruments, a simulation computer, an instrument computer, and a switch connected with simulation computer network equipment and instrument computer network equipment. The simulation computer can obtain display data of the instruments in the cockpit according to a simulation model of an aircraft system and transmit the display data to the instrument computer through a UDP (user datagram protocol), and the instrument computer can drive virtual instruments to realize real-time display of the state of an aircraft by output data of the simulation computer. The platform can realize real-time display of dynamic simulation data by the virtual instruments according to a simulation result of the model of the aircraft system and has the advantages of high fidelity and low cost.
Description
Technical field
The invention discloses the aircraft cockpit digital simulation manoeuvring platform of semi physical, belong to the technical field that the aircraft simulation is handled.
Background technology
The aircraft cockpit digital simulation manoeuvring platform of semi physical is to realize the necessary manoeuvring platform of people at the loop flight simulation, it is the necessary assembly of realizing simulated flight and instrumentation engineering simulating developer, instrument simulation one class is to adopt boat material instrument to reequip realization at present, cost is high, interface data is huge, install complicated, the enforcement difficulty is large, especially often because obtaining complete bus data definition, realize difficulty for the instrument simulation of external aircraft, the another kind of instrument simulation interface that is based on simple construction, the data-driven that lacks the aircraft system realistic model, can't carry out the flight simulation of aircraft complete section face, therefore, be badly in need of a kind of dependence PC environment and software emulation technology, the aircraft cockpit digital simulation manoeuvring platform of the semi physical of realizing with aircraft system realistic model data-driven.
Summary of the invention
Technical matters to be solved by this invention is the deficiency for the above-mentioned background technology, and the aircraft cockpit digital simulation manoeuvring platform of semi physical is provided.
The present invention adopts following technical scheme for achieving the above object:
The aircraft cockpit digital simulation manoeuvring platform of semi physical comprises:
For the pilot provides the driving cabin visual system of simulated flight what comes into a driver's,
In simulator cockpit, the pilot takes the flight control device that settle in space,
Gather the data acquisition system (DAS) of flight control device manipulation data,
Be placed in showing for the touch of Displaying Meter data in real time in simulator cockpit and in center pedestal
Show device,
Handle input data, aircraft flight data according to the flight control device, binding kinetics equation, aircraft system realistic model obtain the simulation computer that virtual instrument shows data,
For the treatment of virtual instrument show data obtain instrument show in real time data instrument computer,
The switch that connects the simulation computer network equipment, the instrument computer network equipment.
In the aircraft cockpit digital simulation manoeuvring platform of described semi physical, instrument computer utilizes GL studio software processing virtual instrument to show that data obtain instrument and show in real time data.
In the aircraft cockpit digital simulation manoeuvring platform of described semi physical, the driving cabin visual system is according to aspect and ground scape database generating three-dimensional picture.
The aircraft cockpit digital simulation manoeuvring platform of described semi physical is realized the method that the virtual instrument data show, specifically comprises the steps:
Step 1, simulation computer, according to flying quality and the kinetics equation of aircraft, is set up the aircraft system realistic model;
Step 2, obtain and handle the input data by data acquisition system (DAS);
Step 3, the manipulation input data that simulation computer obtains in conjunction with data acquisition system (DAS), obtain virtual instrument according to the aircraft system realistic model and show data;
Step 4, instrument computer is set up driving cabin instrument model, and the UDP message of take obtains virtual data as inputting data, and driving cabin instrument model generates driving data under Data Transport Protocol;
Step 5, display shows virtual data, used by aviation instrument panel under the driving data effect, show in real time the aircraft longitude and latitude, highly, the angle of rudder reflection data.
The described aircraft cockpit digital simulation manoeuvring platform of semi physical that utilizes is realized the method that the virtual instrument data show, virtual instrument demonstration data are transmitted according to udp protocol.
The present invention adopts technique scheme, has following beneficial effect:
(1) obtain the driving data for instrument simulation according to manipulation assembly manipulation data and the aircraft state parameter of Real-time Collection, realized the dynamic demonstration of instrumented data, made up and can only show the defect of static manipulation data in the prior art, realized the closed-loop simulation of people at loop;
(2) reequip with respect to available technology adopting boat material instrument the instrument simulation of realizing, the present invention has reduced the emulation cost under the prerequisite of the impact of having considered model aircraft emulation.
The accompanying drawing explanation
The configuration diagram of the aircraft cockpit digital simulation manoeuvring platform that Fig. 1 is semi physical.
Fig. 2 is the schematic diagram that virtual instrument system is realized the instrument simulation method.
Embodiment
Technical scheme below in conjunction with accompanying drawing to invention is elaborated.
Semi physical aircraft cockpit digital simulation manoeuvring platform as shown in Figure 1 comprises:
In simulator cockpit, the pilot takes the flight control device that settle in space, and the flight control device comprises control wheel, jociey stick, pedal, throttle platform, mode control panel (MCP) and digital number flying instruments display system (EFIS) etc.;
Gather the data acquisition system (DAS) of flight control device manipulation data, the manipulation data of flight control device is converted into digital quantity through I/O, the A/D circuit of data acquisition system (DAS), through serial ports, is transferred in simulation computer;
According to flight control device manipulation data, aircraft state parameter, in conjunction with Aerodynamics Model, large compression ring
The border realistic model, ground controlling power realistic model, the aircraft system realistic model obtains the simulation computer of driving data, the aircraft system realistic model comprises: the air-conditioning system model, the autoflight system model, the power-supply system model, the fire prevention system model, the flight control system model, the fuel system model, the hydraulic system model, anti-icing rain repellant system model, the Landing Gear System model, Navigation System Model, the air supply system model, the APU system model, engine system models, the aircraft state parameter that the aircraft system realistic model arranges with simulation control subsystem (being the action button of center pedestal), as zero fuel weight, center of gravity, amount of fuel, ground power supply, the ground source of the gas, the aircraft longitude and latitude, highly, ambient wind, the dynamic similation aircraft system,
Be placed in simulator cockpit and the interior display for real-time Displaying Meter data of center pedestal: mould
Three touch display screens intending settling in driving cabin are respectively used to the demonstration of captain's side instrument, copilot side instrument shows and engine parameter shows, two touch displays of center pedestal are respectively used to Mult1purpose Coutrols ＆ Display Unit (MCDU) and lower display module (LDU) shows, needs according to type, the aluminium alloy masking-out is installed on display, the part of exposing needs, cover remainder, make the outward appearance of emulation instrument more approach the type of simulating;
For the pilot provides the driving cabin visual system of simulated flight what comes into a driver's, according to the flight of simulation computer output
Attitude, aircraft longitude and latitude, highly, the data such as angle of rudder reflection, the terrain data generating three-dimensional picture in real-time calling ground scape database, and output to optical projection system and form the what comes into a driver's picture, for the pilot provides comparatively real visual experience;
By driving signal to obtain showing in real time the instrument computer of data, instrument computer utilizes two-dimensional/three-dimensional instrument instrument simulation software as GL Studio, the driving data of take obtains as inputting data simulation the instrumented data shown in real time, by being placed in simulator cockpit and providing the instrument display interface for the real-time display of Displaying Meter data in center pedestal, realize that the data of primary flight display (PFD), navigation indicator (ND), engine parameter display (ED), integrated form standby meter (ISI), wireless electromagnetic indicator (RMI) show;
Primary flight display (PFD) is controlled desired parameters for the flight air route provides dynamic color to show, demonstration comprises: flying method prompting, air speed, highly, vertical speed, attitude, operation information, radio altitude, instrument landing system (ILS) demonstration, decision height, course/flight path indication, TCAS indication and EGPWS indication, aircraft system breaks down all can have failure flag to show;
Navigation shows that (ND) provides colored flight process to show, display mode comprises MAP, APP, VOR and PLN mode, and MAP, VOR and APP pattern can be changed between the center mode of the mode of extension of half compass and full compass.
Engine parameter display (ED) shows temperature, thrust mode, N1 rotating speed and EGT, engine failure alarm and the unit alarm thereof etc. of engine;
Lower display module (LDU) is located at the center pedestal front panel, shows N2 rotating speed, fuel flow, lubricating oil pressure, oil temperature, oil flow and the engine luggine value etc. of engine, can provide extract to press and the flight control system indication simultaneously;
Connect the switch of the simulation computer network equipment, the instrument computer network equipment, the driving data that simulation computer obtains transfers to instrument computer according to udp protocol.
Physical arrangement comprises cabin body case, base, light shield mounting structure, instrument panel, aircraft handling device.The aircraft cockpit digital simulation manoeuvring platform of semi physical, take the cockpit structure of simulated type and instrument layout characteristics is basis, in conjunction with composite factors such as modern emulation technology and applied environments, adopt virtual instrument technology to realize the emulation of instrument, by by atmospheric environment model, Aerodynamics Model, the crosslinked analogue system of the composition of ground controlling power model and aircraft system realistic model provides driving data for virtual instrument, and application instrument simulation software realizes that virtual instrument is picture stimulated, provide display frame by the display be arranged on flying panel and center pedestal, the operation of Reality simulation aircraft and feedback.The flight such as control wheel, pedal Control Component is installed in passenger cabin, and the control panels such as digital flying instruments display system (EFIS) control panel, mode control panel (MCP), realize the flight simulation of people at loop.
The process of the stages such as the aircraft cockpit digital simulation manoeuvring platform of semi physical can simulate and realize the taking off of aircraft, cruises, landing, thus simulate parameter and the show state of instrument stages.Mode control panel (MCP) is mainly used in controlling the DFCS system (digital flight control system) of aircraft, and the working method of selection autoflight system, Pre-select Heading, air speed, height etc., be positioned at the light shield middle part.The EFIS control panel comprises two of left and right, is mainly used in controlling the instrument system of aircraft, and the displaying contents of control PFD, ND, air pressure benchmark, decision height etc., be positioned at the light shield both sides.Control wheel/bar mainly provides the rolling of aircraft and pitch attitude to control.Pedal provides the aircraft driftage to control function and function is controlled in brake.The throttle platform can be realized the control function of engine, comprises thrust handle, anti-pushing handle, spoiler joystick, flap slat joystick, horizontal stabilizer trim wheel, stops brake and fuel-cut handle etc.Above a few part related hardware can intactly be realized driving by I/O, A/D acquisition system in system, and be connected with main control computer by data bus interface, data acquisition resolves by realistic model, effectively send the instrument drive data in each stage of aircraft to the instrument Display control computer, the flight control personnel show according to instrument and current state is carried out follow-up operation, realize complete control procedure.
Virtual instrument system is realized the instrument simulation method as shown in Figure 2, comprises the steps:
Step 1, simulation computer, according to flying quality and the kinetics equation of aircraft, is set up the aircraft system realistic model;
Step 2, obtain and handle the input data by data acquisition system (DAS);
Step 3, the manipulation input data that simulation computer obtains in conjunction with data acquisition system (DAS), obtain virtual instrument according to the aircraft system realistic model and show data;
Step, 4 instrument computers are set up driving cabin instrument model, and the UDP message of take obtains virtual data as inputting data, and driving cabin instrument model generates driving data under Data Transport Protocol;
Step 5, display shows virtual data, used by aviation instrument panel under the driving data effect, show in real time the aircraft longitude and latitude, highly, the data such as angle of rudder reflection.
This simulation manoeuvring platform can receive in real time emulated data and feed back to virtual instrument system, and the signal produced by simulation system sends on instrument computer through network.The designed virtual instrument of native system can meet various forms of two dimensions, three-dimensional instrument exploitation (such as GL Studio, MutiGen Creator, Vega Primer etc.) fully, also can design and develop the true instrument display system that meets the ARINC661 standard.
The driving data of virtual instrument is between different computing machines, to communicate in LAN (Local Area Network).And Windows Socket is for the bottom Windows API of TCP/IP programming, by means of Winsock, can realize preferably netting interior communication.While programming based on Winsock, according to these system actual conditions, mission computer carries out data transmission with the forms of broadcasting, adopts based on UDP(towards connectionless) the Socket programming, client computer is in real time from Network Capture data demonstration.
Adopt the mode of UDP, guaranteed to show the real-time of data, not there will be situations such as making to show hysteresis because of network congestion.For the transmission rate of 20ms/ time, can not affect vision response under the UDP mode, can guarantee that platform realizes real-time response.The target that this simulation manoeuvring platform drives the virtual instrument design to complete is: by the state of flight information of aircraft, comprise that mission phase demonstration, state of flight, engine condition, the rudder face degree of bias, the angle of pitch, roll angle, course angle, lateral deviation move speed, flying height apart from, lateral deviation, the information such as vertical speed, ground velocity, air speed are detailed, reasonably show, especially meet the requirement of true aircraft, realize that the simulating developer of virtual instrument and the exploration of new aircraft instrument design and develop.Attainable EFIS instrument comprises primary flight display (PFD), navigation indicator (ND), engine parameter display (ED), lower display module (LDU) etc.
The aircraft cockpit digital simulation manoeuvring platform of the semi physical the present invention relates in sum, has following beneficial effect:
(1) obtain the driving data for instrument simulation according to manipulation assembly manipulation data and the aircraft state parameter of Real-time Collection, realized the dynamic demonstration of instrumented data, made up and can only show the defect of static manipulation data in the prior art, realized the closed-loop simulation of people at loop;
(2) reequip with respect to available technology adopting boat material instrument the instrument simulation of realizing, the present invention has reduced the emulation cost under the prerequisite of the impact of having considered model aircraft emulation.
Claims (5)
1. the aircraft cockpit digital simulation manoeuvring platform of semi physical comprises:
For the pilot provides the driving cabin visual system of simulated flight what comes into a driver's,
In simulator cockpit, the pilot takes the flight control device that settle in space,
Gather the data acquisition system (DAS) of flight control device manipulation data,
Be placed in showing for the touch of Displaying Meter data in real time in simulator cockpit and in center pedestal
Show device,
It is characterized in that: the flight driving cabin digital simulation manoeuvring platform of described semi physical also comprises:
Handle input data, aircraft flight data according to the flight control device, binding kinetics equation, aircraft system realistic model obtain the simulation computer that virtual instrument shows data,
For the treatment of virtual instrument show data obtain instrument show in real time data instrument computer,
The switch that connects the simulation computer network equipment, the instrument computer network equipment.
2. the aircraft cockpit digital simulation manoeuvring platform of semi physical according to claim 1 is characterized in that: described instrument computer utilizes GL studio software to process virtual instrument to show that data obtain instrument and show in real time data.
3. the aircraft cockpit digital simulation manoeuvring platform of semi physical according to claim 1 and 2 is characterized in that: described driving cabin visual system is according to aspect and ground scape database generating three-dimensional picture.
4. utilize the aircraft cockpit digital simulation manoeuvring platform of claim 1 or 2 described semi physical to realize the method that the virtual instrument data show, it is characterized in that: specifically comprise the steps:
Step 1, simulation computer, according to flying quality and the kinetics equation of aircraft, is set up the aircraft system realistic model;
Step 2, obtain and handle the input data by data acquisition system (DAS);
Step 3, the manipulation input data that simulation computer obtains in conjunction with data acquisition system (DAS), obtain virtual instrument according to the aircraft system realistic model and show data;
Step, 4 instrument computers are set up driving cabin instrument model, and the UDP message of take obtains virtual data as inputting data, and driving cabin instrument model generates driving data under Data Transport Protocol;
Step 5, display shows virtual data, used by aviation instrument panel under the driving data effect, show in real time the aircraft longitude and latitude, highly, the angle of rudder reflection data.
5. the aircraft cockpit digital simulation manoeuvring platform of semi physical that utilizes according to claim 4 is realized the method that the virtual instrument data show, it is characterized in that, described virtual instrument demonstration data are transmitted according to udp protocol.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2013103836699A CN103473966A (en) | 2013-08-29 | 2013-08-29 | Semi-physical digital simulation control platform of aircraft cockpit |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2013103836699A CN103473966A (en) | 2013-08-29 | 2013-08-29 | Semi-physical digital simulation control platform of aircraft cockpit |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103473966A true CN103473966A (en) | 2013-12-25 |
Family
ID=49798792
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2013103836699A Pending CN103473966A (en) | 2013-08-29 | 2013-08-29 | Semi-physical digital simulation control platform of aircraft cockpit |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103473966A (en) |
Cited By (26)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103871292A (en) * | 2014-03-27 | 2014-06-18 | 芜湖航飞科技股份有限公司 | Full-function flight simulator |
| CN103886783A (en) * | 2014-03-18 | 2014-06-25 | 西京学院 | Real-time analogue simulation system of aviation piloting instrument |
| CN104269083A (en) * | 2014-09-04 | 2015-01-07 | 吉林医药学院 | Low-cost flight simulator cabin display and control system |
| CN105539854A (en) * | 2016-01-21 | 2016-05-04 | 南京航空航天大学 | Cockpit driving work efficiency designing and evaluating system platform |
| CN105632271A (en) * | 2016-03-04 | 2016-06-01 | 中国空气动力研究与发展中心低速空气动力研究所 | Ground simulation training system for low-speed wind tunnel model flight experiment |
| CN105699103A (en) * | 2014-11-28 | 2016-06-22 | 上海航空电器有限公司 | Portable enhanced ground proximity alarm system test device |
| CN107102565A (en) * | 2017-06-03 | 2017-08-29 | 复旦大学 | Unmanned plane clustered software assemblage on-orbit system |
| 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 |
| CN107515587A (en) * | 2017-08-30 | 2017-12-26 | 工业和信息化部电子第五研究所华东分所 | System, method, apparatus, equipment and the storage medium of man-machine interactive operation emulation |
| CN107909883A (en) * | 2017-11-03 | 2018-04-13 | 中国民用航空飞行学院 | Robinson's R44 helicopter multitask flight training devices |
| CN108288416A (en) * | 2018-03-21 | 2018-07-17 | 哈尔滨莱特兄弟飞行技术有限公司 | A kind of simulation aircraft fire protection control panel manipulation device |
| CN109188934A (en) * | 2018-11-15 | 2019-01-11 | 中国民航大学 | The analogue system and method for avionics system power supply, information data processing terminal |
| CN109215436A (en) * | 2018-11-05 | 2019-01-15 | 成都泛美视界科技有限公司 | A kind of teacher station system towards flight simulation training |
| 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 |
| CN110531978A (en) * | 2019-07-11 | 2019-12-03 | 北京机电工程研究所 | A kind of cockpit display system |
| CN110910709A (en) * | 2019-10-09 | 2020-03-24 | 成都艾尔伯特科技有限责任公司 | Simulation avionics system |
| CN111158261A (en) * | 2019-12-17 | 2020-05-15 | 西北工业大学 | Simulation method and system of airplane control system |
| CN112764355A (en) * | 2020-12-05 | 2021-05-07 | 西安翔腾微电子科技有限公司 | Vision-based aircraft autonomous landing positioning development system and method |
| CN113419509A (en) * | 2021-05-26 | 2021-09-21 | 中国航空工业集团公司沈阳飞机设计研究所 | Aircraft automatic control subassembly test system |
| CN113470476A (en) * | 2021-08-20 | 2021-10-01 | 沈阳飞机工业（集团）有限公司 | Dynamic simulation training operating platform of airplane control system and using method |
| CN114019939A (en) * | 2021-11-03 | 2022-02-08 | 商飞软件有限公司 | Civil aircraft cockpit distributed simulation system |
| CN114373359A (en) * | 2021-12-10 | 2022-04-19 | 厦门提坦航电科技有限公司 | Aircraft cockpit control method and device and readable medium |
| CN114491818A (en) * | 2022-03-03 | 2022-05-13 | 中国人民解放军91475部队 | Simulated flight system of transport vehicle |
| CN114970094A (en) * | 2022-04-19 | 2022-08-30 | 北京电子工程总体研究所 | Control and automatic maneuver simulation system and method applied to cluster fighter scene |
| CN115331515A (en) * | 2022-07-26 | 2022-11-11 | 浙江大学苏州工业技术研究院 | Lightweight online flight simulation system based on enhanced virtual reality |
| 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 (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101794523A (en) * | 2009-12-15 | 2010-08-04 | 中国民航大学 | Aircraft hardware-in-the-loop simulation device |
| CN202422464U (en) * | 2011-12-27 | 2012-09-05 | 安徽鑫众信息技术有限公司 | Visual simulation airplane |
| CN103065022A (en) * | 2013-01-24 | 2013-04-24 | 无锡华航电子科技有限责任公司 | Incentive model simulation platform for aerocraft electronic system |
-
2013
- 2013-08-29 CN CN2013103836699A patent/CN103473966A/en active Pending
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101794523A (en) * | 2009-12-15 | 2010-08-04 | 中国民航大学 | Aircraft hardware-in-the-loop simulation device |
| CN202422464U (en) * | 2011-12-27 | 2012-09-05 | 安徽鑫众信息技术有限公司 | Visual simulation airplane |
| CN103065022A (en) * | 2013-01-24 | 2013-04-24 | 无锡华航电子科技有限责任公司 | Incentive model simulation platform for aerocraft electronic system |
Cited By (37)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103886783A (en) * | 2014-03-18 | 2014-06-25 | 西京学院 | Real-time analogue simulation system of aviation piloting instrument |
| CN103886783B (en) * | 2014-03-18 | 2016-04-27 | 西京学院 | A kind of aviation control instruments real-time analog simulation system |
| CN103871292B (en) * | 2014-03-27 | 2017-01-18 | 芜湖航飞科技股份有限公司 | Full-function flight simulator |
| CN103871292A (en) * | 2014-03-27 | 2014-06-18 | 芜湖航飞科技股份有限公司 | Full-function flight simulator |
| CN104269083A (en) * | 2014-09-04 | 2015-01-07 | 吉林医药学院 | Low-cost flight simulator cabin display and control system |
| CN105699103A (en) * | 2014-11-28 | 2016-06-22 | 上海航空电器有限公司 | Portable enhanced ground proximity alarm system test device |
| CN105699103B (en) * | 2014-11-28 | 2018-12-25 | 上海航空电器有限公司 | A kind of portable enhanced ground proximity warning system test equipment |
| CN105539854B (en) * | 2016-01-21 | 2018-08-24 | 南京航空航天大学 | A kind of aircraft cockpit drives ergonomics and assessment system platform |
| CN105539854A (en) * | 2016-01-21 | 2016-05-04 | 南京航空航天大学 | Cockpit driving work efficiency designing and evaluating system platform |
| CN105632271A (en) * | 2016-03-04 | 2016-06-01 | 中国空气动力研究与发展中心低速空气动力研究所 | Ground simulation training system for low-speed wind tunnel model flight experiment |
| CN107102565A (en) * | 2017-06-03 | 2017-08-29 | 复旦大学 | Unmanned plane clustered software assemblage on-orbit system |
| 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 |
| 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 |
| CN107515587A (en) * | 2017-08-30 | 2017-12-26 | 工业和信息化部电子第五研究所华东分所 | System, method, apparatus, equipment and the storage medium of man-machine interactive operation emulation |
| CN107515587B (en) * | 2017-08-30 | 2020-07-07 | 工业和信息化部电子第五研究所华东分所 | System, method, device, equipment and storage medium for man-machine interaction operation simulation |
| CN107909883A (en) * | 2017-11-03 | 2018-04-13 | 中国民用航空飞行学院 | Robinson's R44 helicopter multitask flight training devices |
| CN108288416A (en) * | 2018-03-21 | 2018-07-17 | 哈尔滨莱特兄弟飞行技术有限公司 | A kind of simulation aircraft fire protection control panel manipulation device |
| CN108288416B (en) * | 2018-03-21 | 2024-04-02 | 哈尔滨莱特兄弟科技开发有限公司 | Control device for simulating fireproof control panel of airplane |
| CN109215436A (en) * | 2018-11-05 | 2019-01-15 | 成都泛美视界科技有限公司 | A kind of teacher station system towards flight simulation training |
| CN109188934A (en) * | 2018-11-15 | 2019-01-11 | 中国民航大学 | The analogue system and method for avionics system power supply, information data processing terminal |
| CN110531978A (en) * | 2019-07-11 | 2019-12-03 | 北京机电工程研究所 | A kind of cockpit display system |
| CN110531978B (en) * | 2019-07-11 | 2023-11-03 | 北京机电工程研究所 | Cabin display 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 |
| CN110910709A (en) * | 2019-10-09 | 2020-03-24 | 成都艾尔伯特科技有限责任公司 | Simulation avionics system |
| CN111158261A (en) * | 2019-12-17 | 2020-05-15 | 西北工业大学 | Simulation method and system of airplane control system |
| CN112764355B (en) * | 2020-12-05 | 2022-12-13 | 西安翔腾微电子科技有限公司 | Vision-based autonomous landing positioning development system and method for airplane |
| CN112764355A (en) * | 2020-12-05 | 2021-05-07 | 西安翔腾微电子科技有限公司 | Vision-based aircraft autonomous landing positioning development system and method |
| CN113419509A (en) * | 2021-05-26 | 2021-09-21 | 中国航空工业集团公司沈阳飞机设计研究所 | Aircraft automatic control subassembly test system |
| CN113470476A (en) * | 2021-08-20 | 2021-10-01 | 沈阳飞机工业（集团）有限公司 | Dynamic simulation training operating platform of airplane control system and using method |
| CN114019939A (en) * | 2021-11-03 | 2022-02-08 | 商飞软件有限公司 | Civil aircraft cockpit distributed simulation system |
| CN114373359A (en) * | 2021-12-10 | 2022-04-19 | 厦门提坦航电科技有限公司 | Aircraft cockpit control method and device and readable medium |
| CN114373359B (en) * | 2021-12-10 | 2024-04-30 | 厦门提坦航电科技有限公司 | Method and device for controlling aircraft cockpit and readable medium |
| CN114491818A (en) * | 2022-03-03 | 2022-05-13 | 中国人民解放军91475部队 | Simulated flight system of transport vehicle |
| CN114491818B (en) * | 2022-03-03 | 2024-09-06 | 中国人民解放军91475部队 | Simulated flight system of conveyor |
| CN114970094A (en) * | 2022-04-19 | 2022-08-30 | 北京电子工程总体研究所 | Control and automatic maneuver simulation system and method applied to cluster fighter scene |
| 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 |
| CN115331515A (en) * | 2022-07-26 | 2022-11-11 | 浙江大学苏州工业技术研究院 | Lightweight online flight simulation system based on enhanced virtual reality |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN103473966A (en) | Semi-physical digital simulation control platform of aircraft cockpit | |
| Allerton | The impact of flight simulation in aerospace | |
| CN103871292B (en) | Full-function flight simulator | |
| US20090220929A1 (en) | Pc-based simulator training system and methods | |
| CN113496635B (en) | Flight simulator and flight training simulation method | |
| WO2005109375A1 (en) | Recurrent training full flight simulators | |
| US20110207091A1 (en) | Compact multi-aircraft configurable flight simulator | |
| CN112164274A (en) | Aircraft flight control simulation system | |
| Viertler et al. | Requirements and design challenges in rotorcraft flight simulations for research applications | |
| Andreev et al. | Information models for designing conceptual broad-profile flight simulators | |
| CN207780525U (en) | A kind of synthesis avionics simulation system for helicopter measures of effectiveness | |
| CN116312136A (en) | Aircraft cabin simulation system and fault simulation training method thereof | |
| Coiro et al. | A 6dof flight simulation environment for general aviation aircraft with control loading reproduction | |
| Ackerman et al. | Pilot-in-the-loop flight simulator for NASA’s Transport Class Model | |
| WO2023084456A1 (en) | System for simulating the operation of a vehicle, associated components and methods | |
| Balcerzak et al. | Flight Simulation in Civil Aviation: advantages and disadvantages. | |
| Cameron et al. | Tilt Rotor Pitch/Flight‐Path Handling Qualities | |
| Gaublomme et al. | Using Virtual Simulation to Enhance Rotorcraft Shipboard Flight Testing | |
| Yurkov et al. | Designing aircraft simulators | |
| Chudy et al. | Intuitive flight display for light aircraft. | |
| Zheng et al. | Semi-Physical Simulation Design of UAV Simulation Training System | |
| Taylan et al. | Mathematical Modelling, Simulation and Application of Full Flight Helicopter Simulator | |
| Memon | The development of high-fidelity modelling & simulation for the helicopter ship dynamic interface | |
| RU141896U1 (en) | TRAINING AND MODELING COMPLEX OF FLIGHT COMPOSITION AND SPECIALISTS OF AIRCRAFT MANAGEMENT | |
| Reardon et al. | Scenario Development Process at the Vertical Motion 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 | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20131225 |