CN101976278A - Virtual reality technique-based airplane landing aid system and method thereof - Google Patents

Virtual reality technique-based airplane landing aid system and method thereof Download PDF

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Publication number
CN101976278A
CN101976278A CN2010105000781A CN201010500078A CN101976278A CN 101976278 A CN101976278 A CN 101976278A CN 2010105000781 A CN2010105000781 A CN 2010105000781A CN 201010500078 A CN201010500078 A CN 201010500078A CN 101976278 A CN101976278 A CN 101976278A
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landing
aircraft
virtual reality
pilot
airplane
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CN2010105000781A
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CN101976278B (en
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张凯
朱洪涛
叶鼎晟
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Nanjing University of Information Science and Technology
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Nanjing University of Information Science and Technology
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Abstract

The invention discloses a virtual reality technique-based airplane smooth landing aid system and a method thereof, belonging to the field of aviation service. The system of the invention comprises a data acquisition module, a virtual reality processing module and a display module. The method of the invention includes that: when an airplane is landing, a real-time pictures of relative position between the current airport road surface and airplane landing wheels are simulated at a control terminal by adopting virtual reality technique and combining an airport road surface real-time picture and airplane landing wheel sensor data. The real-time pictures are beneficial for a pilot to operate and judge, thus judging of the pilot on flight path and airplane position can be more visual. According to real-time relative position, optimal place, optimal angle and optimal speed for landing are obtained by terminal simulation, so as to aid the pilot to realize smooth landing of airplane.

Description

Aircraft landing backup system and method based on virtual reality technology
Technical field
The present invention relates to aircraft stable landing control method, belong to Aeronautical Service field and computer simulation emulation field based on virtual reality technology.
Background technology
Along with making rapid progress of space flight and aviation technology, aircraft more and more becomes a kind of indispensable vehicles of modern society, safe take-off for aircraft, flight has also had new definition and requirement with landing, thereby this case has proposed a kind of aircraft stable landing method based on virtual reality technology, realizes more steady and safe aircraft landing with assisting in flying person.
Aircraft landing in the past mainly relies on pilot's experience and the auxiliary of instrument numerical value to land, and on the near-earth height, judge that aircraft altitude and rate of descent should be to observe the storehouse external environment, numerical value shown in the instrument this moment out of true and hysteresis is arranged, only can be used as reference, therefore cause the landing shakiness of aircraft unavoidably.And great aircraft accident, great majority are in the near landing process at aircraft and take place, particularly run into the meteorological trap that forms under the IFR conditions, be that horizontal visibility meets aerodrome op erating minimum, but the pilot is in advancing nearly landing process, and the slant visibility of in fact seeing is very poor, can not on decision height, in time find and when aiming at airfield runway, cause a serious accident easily.
The landing process: main frame was taken turns before this, and just the back undercarriage lands earlier; Because will have one to draw the journey of sailing (head raises up, and motor power is reduced to minimum) at last at aircraft landing, for before landing, reduce buffering exactly, reduce sinking speed, thereby impulsive force is to the destruction of body when reducing to land.Be that nosewheel lands at last, just nose-gear lands.The back undercarriage landed, was nose-gear then before this.Therefore the research of just controlling for the research of aircraft stable landing for the aircraft landing wheel.
Summary of the invention
Technical matters to be solved by this invention is some defectives that exist at current aircraft landing smoothness, a kind of aircraft stable landing method based on virtual reality technology that provides.
The present invention adopts following technical scheme for achieving the above object:
The present invention is based on the aircraft stable landing backup system of virtual reality technology, comprise display module in data acquisition module, virtual reality processing module and the cabin, the pilot is the operator of described system, the pilot starts described system, data acquisition module BOB(beginning of block) image data also is sent to the virtual reality processing module with the data of gathering and is handled, and the view data that the virtual reality processing module is handled shows in the display module with assisting in flying person in the cabin carries out the landing operation.
Preferably, the computing machine in the described virtual reality processing module receives the aircraft landing wheel of the sensor that is installed on the aircraft landing wheel and the signal of ground distance, is created on the virtual scene of aircraft and ground distance.
Control method based on the aircraft stable landing backup system of virtual reality technology comprises the steps:
1) when aircraft advances near landing, the pilot opens the landing backup system;
2) laser range sensor that is positioned on the aircraft landing wheel is started working, and landing wheel and ground interplanar distance are sent to computing machine in the virtual reality processing module from data;
3) computer run virtual reality software, by the range data between landing wheel that receives and the ground simulate aircraft with ground relation of plane virtual scene;
4) virtual scene that is gone out by the virtual reality software simulation shows in the display in the cabin, and the pilot selects best landing scheme according to aircraft that provides in the virtual scene and ground relation, to realize the stable landing of aircraft.
The present invention with the operation of common landing in the past different be, in the past landing operation all be carry out according to pilot's flying experience even up, flatly waft, ground connection, on the near-earth height, judged in the past that aircraft altitude and rate of descent all were based on the astrodome external environment, and the simulation of the extravehicular environment that demonstrates by virtual reality technology, can give the pilot reference that gets aircraft altitude and rate of descent the most directly perceived, solve in the past ubiquitous problem in the aircraft landing, therefore must realize the stable landing of aircraft to the full extent.
Description of drawings
Fig. 1 is a system module composition diagram of the present invention;
Fig. 2 is a workflow diagram of the present invention;
Fig. 3 is the workflow diagram of virtual reality processing module;
Fig. 4 is a horizontal virtual reality image in the display in the cabin;
Fig. 5 is a vertical virtual reality image in the display in the cabin.
Embodiment
Be elaborated below in conjunction with the technical scheme of accompanying drawing to invention:
In Fig. 1, display module in virtual reality module, data acquisition module, the cabin, all be to finish by the hardware facility that is installed on the aircraft, the pilot is the startup person and the effector of system.The main modular of system is the virtual reality module, it is sent to the real time modelling image of actual environment the display of being presented in face of the pilot, can allow the true change in location that must experience aircraft with respect to the airport of pilot, help that the pilot is better must to finish the landing process, realize the aircraft stable landing.
Fig. 2 and Fig. 3 are based on the workflow diagram of the aircraft stable landing method of virtual reality technology.
At first, when aircraft advanced near landing, the pilot started auxiliary landing system, promptly realized the stable landing of aircraft by virtual reality technology.
Secondly, computer run virtual reality software, the range data of comprehensively passing back and be pre-stored in airport and airplane data in the computing machine simulates the relative position of current aircraft and airfield runway, finishes virtual reality.Be the workflow diagram of virtual reality processing module as shown in Figure 3, when the pilot opens this auxiliary landing system, computing machine is earlier according to the airport data that are preset in the internal memory, finish the generation of airport environment, and the aircraft three-dimensional model of in the scene of airport, packing into, distance measuring sensor is set starts working, this has just finished the initialization for this system virtualization reality.Enter the instant virtual process of computing machine then for reality, computing machine reads the landing wheel that records and the distance between the ground, actual range and the relation of the distance proportion in the three-dimensional scenic according to measuring and calculating in advance, draw model aircraft new position data in scene, upgrade the position of three-dimensional model aircraft with respect to the airport virtual scene.After having finished the once renewal for the aircraft three-dimensional model, read the distance measuring sensor data once more, up to the aircraft stable landing, the pilot closes the landing backup system.
Once more as shown in Figure 4 and Figure 5, the virtual reality picture is presented on the display of driving cabin control panel.Obviously the analog image that generates by virtual reality not only can be clearly seen that overall aircraft with respect to the airfield runway position, but also whether the landing wheel is positioned on the same surface level after can observing two.The observation overall aircraft is with respect to the meaning of airfield runway position: determine aircraft aircraft elevation angle in the flat journey of sailing intuitively, if the elevation angle then empennage bigger than normal contacts to earth, cause the landing failure, the elevation angle then back landing less than normal wheel can't contact to earth earlier, also cause the landing failure, therefore by the image of overall aircraft with respect to airfield runway, the pilot can intuitively must judge the aircraft elevation angle, and in time handle, select the best elevation angle; To guarantee the stable landing of aircraft; Observe back landing wheel whether the meaning on same horizontal line be: after gear down, whether the landing wheel has just determined the stable landing of aircraft after two on same surface level, if two landing wheels are not on same surface level, do not land simultaneously owing to left and right wheels during landing, just can cause the vibrations of fuselage, the serious aircraft that also can cause guns off the runway, by the virtual reality image, can intuitively must observe left and right wheels the position, assisting in flying person finishes the stable landing of aircraft; At last, the pilot carries out the landing operation.

Claims (3)

1. aircraft stable landing backup system based on virtual reality technology, it is characterized in that this system comprises display module in data acquisition module, virtual reality processing module and the cabin, the pilot is the operator of described system, the pilot starts described system, data acquisition module BOB(beginning of block) image data also is sent to the virtual reality processing module with the data of gathering and is handled, and the view data that the virtual reality processing module is handled shows in the display module with assisting in flying person in the cabin carries out the landing operation.
2. the aircraft stable landing control system based on virtual reality technology according to claim 1, it is characterized in that the computing machine in the described virtual reality processing module receives the aircraft landing wheel of the sensor that is installed on the aircraft landing wheel and the signal of ground distance, is created on the virtual scene of aircraft and ground distance.
3. the control method based on the described aircraft stable landing backup system based on virtual reality technology of claim 1 is characterized in that comprising the steps:
1) when aircraft advances near landing, the pilot opens the landing backup system;
2) laser range sensor that is positioned on the aircraft landing wheel is started working, and landing wheel and ground interplanar distance are sent to computing machine in the virtual reality processing module from data;
3) computer run virtual reality software, by the range data between landing wheel that receives and the ground simulate aircraft with ground relation of plane virtual scene;
4) virtual scene that is gone out by the virtual reality software simulation shows in the display in the cabin, and the pilot selects best landing scheme according to aircraft that provides in the virtual scene and ground relation, to realize the stable landing of aircraft.
CN201010500078.1A 2010-09-29 2010-09-29 Virtual reality technique-based airplane landing aid system and method thereof Expired - Fee Related CN101976278B (en)

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Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102054380A (en) * 2010-12-16 2011-05-11 成都西麦克虚拟现实电子技术有限公司 Configurable virtual avionic system
CN103287584A (en) * 2012-03-01 2013-09-11 上海工程技术大学 Video-assisted system for airplane landing
CN104006790A (en) * 2013-02-21 2014-08-27 成都海存艾匹科技有限公司 Vision-Based Aircraft Landing Aid
CN104163245A (en) * 2013-05-15 2014-11-26 空中客车运营简化股份公司 Method and device for displaying the performance of an aircraft when climbing and/or descending
CN105531748A (en) * 2013-09-12 2016-04-27 国立研究开发法人宇宙航空研究开发机构 Landing decision assistance system, landing decision assistance method, and landing decision assistance program
CN106323332A (en) * 2016-08-09 2017-01-11 安庆建金智能科技有限公司 Airplane-descending auxiliary device with laser detection device
CN109062078A (en) * 2018-08-13 2018-12-21 中国科学院长春光学精密机械与物理研究所 VTOL fixed-wing system for flight control computer simulation test platform
CN109507686A (en) * 2018-11-08 2019-03-22 歌尔科技有限公司 A kind of control method wears display equipment, electronic equipment and storage medium
CN109613929A (en) * 2018-12-12 2019-04-12 北京卫星信息工程研究所 A kind of flight precision approach and landing concept and system
CN110503001A (en) * 2019-07-25 2019-11-26 青岛小鸟看看科技有限公司 A kind of Virtual Reality equipment and its barrier-avoiding method, device
CN112960128A (en) * 2021-03-26 2021-06-15 广东汇天航空航天科技有限公司 Auxiliary landing method and device for airplane
CN113212789A (en) * 2021-06-16 2021-08-06 王宇灿 Auxiliary system for airplane taxiing
CN113970933A (en) * 2021-10-22 2022-01-25 中航通飞华南飞机工业有限公司 Water surface landing auxiliary system of seaplane and control method

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106251734B (en) * 2016-10-12 2018-10-02 快创科技(大连)有限公司 A kind of vehicle drive training and examination system based on virtual reality technology

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1356675A (en) * 2001-12-21 2002-07-03 北京航空航天大学 Analog flight training equipment for manipulator of robot helicopter

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1356675A (en) * 2001-12-21 2002-07-03 北京航空航天大学 Analog flight training equipment for manipulator of robot helicopter

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
戴中兴等: "基于视觉的小型垂直起降UAV降落引导技术", 《广州大学学报(自然科学版)》 *

Cited By (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102054380A (en) * 2010-12-16 2011-05-11 成都西麦克虚拟现实电子技术有限公司 Configurable virtual avionic system
CN103287584A (en) * 2012-03-01 2013-09-11 上海工程技术大学 Video-assisted system for airplane landing
CN103287584B (en) * 2012-03-01 2015-12-16 上海工程技术大学 A kind of aircraft video landing ancillary system
CN104006790A (en) * 2013-02-21 2014-08-27 成都海存艾匹科技有限公司 Vision-Based Aircraft Landing Aid
WO2014127607A1 (en) * 2013-02-21 2014-08-28 Zhang Guobiao Visual perception-based airplane landing assisting device
CN104163245A (en) * 2013-05-15 2014-11-26 空中客车运营简化股份公司 Method and device for displaying the performance of an aircraft when climbing and/or descending
CN105531748A (en) * 2013-09-12 2016-04-27 国立研究开发法人宇宙航空研究开发机构 Landing decision assistance system, landing decision assistance method, and landing decision assistance program
CN106323332A (en) * 2016-08-09 2017-01-11 安庆建金智能科技有限公司 Airplane-descending auxiliary device with laser detection device
CN109062078A (en) * 2018-08-13 2018-12-21 中国科学院长春光学精密机械与物理研究所 VTOL fixed-wing system for flight control computer simulation test platform
CN109507686A (en) * 2018-11-08 2019-03-22 歌尔科技有限公司 A kind of control method wears display equipment, electronic equipment and storage medium
CN109507686B (en) * 2018-11-08 2021-03-30 歌尔光学科技有限公司 Control method, head-mounted display device, electronic device and storage medium
CN109613929A (en) * 2018-12-12 2019-04-12 北京卫星信息工程研究所 A kind of flight precision approach and landing concept and system
CN109613929B (en) * 2018-12-12 2022-11-25 北京卫星信息工程研究所 Flight precision approach and landing method and system
CN110503001A (en) * 2019-07-25 2019-11-26 青岛小鸟看看科技有限公司 A kind of Virtual Reality equipment and its barrier-avoiding method, device
CN112960128A (en) * 2021-03-26 2021-06-15 广东汇天航空航天科技有限公司 Auxiliary landing method and device for airplane
CN112960128B (en) * 2021-03-26 2022-11-22 广东汇天航空航天科技有限公司 Auxiliary landing method and device for airplane
CN113212789A (en) * 2021-06-16 2021-08-06 王宇灿 Auxiliary system for airplane taxiing
CN113970933A (en) * 2021-10-22 2022-01-25 中航通飞华南飞机工业有限公司 Water surface landing auxiliary system of seaplane and control method
CN113970933B (en) * 2021-10-22 2024-04-30 中航通飞华南飞机工业有限公司 Water plane water surface landing auxiliary system and control method

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