Virtual three-dimensional landing landmark auxiliary landing method

An assisted landing, virtual three-dimensional technology, applied in the field of synthetic vision and airborne information processing, can solve the problems of not being able to fully recognize the macro environment of the landing area, pilots losing visual reference clues, threatening flight safety, etc., to achieve enhanced credibility Acceleration, enhanced environmental awareness, and reduced landing pressure

Active Publication Date: 2021-01-05
西安应用光学研究所
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] Landing is a routine operation of rotorcraft, and it is also a stage where accidents frequently occur, especially in loose soil or snowy environments. When the helicopter descends vertically to a position close to the ground, the downwash airflow will cause serious dust or snow blindness. As a result, pilots lose external visual reference cues, relying solely on visual flight rules, cannot comprehensively recognize the macro-environment of the landing area, and face potential landing threats (such as grass, snow-covered pits, raised obstacles, etc.) ), if the pilot makes wrong choices and operations based on this, it will seriously threaten his own flight safety, and even lead to the crash of the aircraft

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  • Virtual three-dimensional landing landmark auxiliary landing method
  • Virtual three-dimensional landing landmark auxiliary landing method
  • Virtual three-dimensional landing landmark auxiliary landing method

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Embodiment Construction

[0030] In order to make the purpose, content and advantages of the present invention clearer, the specific implementation manners of the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments.

[0031] Such as figure 1 As shown, the present invention firstly provides a virtual three-dimensional landing landmark assisted landing system, which includes a landing selector module 101 , a landing zone guidance module 102 , a three-dimensional landing landmark module 103 and a data fusion module 104 .

[0032] figure 2 Schematic illustration of the 3D landing landmark assisted landing landing process.

[0033] Step 201: the pilot starts the landing procedure;

[0034] Step 202: The pilot initializes and locates the expected landing point and the landing approach azimuth through the landing selector 101;

[0035] Step 203: After the landing selector 101 is locked, the landing zone guidance module 102 then displays...

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Abstract

The invention discloses a virtual three-dimensional landing landmark auxiliary landing method. The method comprises a landing point selection module, a landing area guiding module, a three-dimensionallanding landmark module and a data fusion module. The landing point selection module is used for providing a man-machine interaction interface for autonomously selecting a landing point for a pilot in a landing selection stage; the landing area guiding module is used for providing landing area prompts with obvious vision and landing approach path guiding for pilots in a landing guiding stage; thethree-dimensional landing landmark module is used for providing spatial position reference for a pilot in the landing process in the landing stage; and the data fusion module fuses and displays the laser radar data and the three-dimensional landing landmark in the form of 8 * 8 grids, so that the environmental perception ability of the landing area of the pilot under the condition that the visualclue is limited is enhanced. The method is clear, visual and convenient to understand, and assists in safe landing of the helicopter.

Description

technical field [0001] The invention belongs to the technical field of airborne information processing and synthetic vision, and relates to a virtual three-dimensional landing landmark assisted landing method. Background technique [0002] Landing is a routine operation of rotorcraft, and it is also a stage where accidents frequently occur, especially in loose soil or snowy environments. When the helicopter descends vertically to a position close to the ground, the downwash airflow will cause serious dust or snow blindness. As a result, pilots lose external visual reference cues, relying solely on visual flight rules, cannot comprehensively recognize the macro-environment of the landing area, and face potential landing threats (such as grass, snow-covered pits, raised obstacles, etc.) ), if the pilot makes wrong choices and operations based on this, it will seriously threaten his own flight safety, and even lead to the crash of the aircraft. [0003] Modern synthetic vision...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G08G5/02
CPCG08G5/025
Inventor 范浩硕高强孙毓凯陶忠杨光李良福安学智张鹏张鑫诚何鹏
Owner 西安应用光学研究所
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