Autonomous control method for fixed point landing of shipboard unmanned aerial vehicle

A control method and autonomous control technology, applied in the field of aviation flight control

Active Publication Date: 2018-12-25
CHENGDU AIRCRAFT INDUSTRY GROUP
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The main purposes of the present invention are as follows: ① solve the problem of smooth transition of the ship-borne UAV from the approach level flight section to the landing glide section; ② solve the problem of the ship-borne UAV accurately tracking the landing glide line; The problem that the nose of the aircraft is aligned with the center line of the runway when it lands

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  • Autonomous control method for fixed point landing of shipboard unmanned aerial vehicle
  • Autonomous control method for fixed point landing of shipboard unmanned aerial vehicle
  • Autonomous control method for fixed point landing of shipboard unmanned aerial vehicle

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Embodiment Construction

[0105] An autonomous control method for fixed-point landing of a ship-borne unmanned aerial vehicle, characterized in that: it includes a control method for a height guidance section, a control method for a two-dimensional guidance section, and a control method for a terminal guidance section; During the entire landing process, first enter the altitude guidance section, track the glide trajectory through the control method of the altitude guidance section, and perform rough trajectory adjustment; enter the two-dimensional guidance section at a height of 200m relative to the airport, and pass the control method of the two-dimensional guidance section The method realizes the precise tracking of the trajectory; when the relative height of the airport is 15m, it enters the terminal guidance section, and through the control method of the terminal guidance section, the nose of the UAV is aligned with the centerline of the runway when it lands.

[0106] The control method of the altit...

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Abstract

Disclosed is an autonomous control method for fixed point landing of shipboard unmanned aerial vehicles. The autonomous control method is characterized in that the autonomous control method comprisesa control method of a height guiding section, a control method of a two-dimensional guiding section, and a control method of a tail end guiding section; a shipborne unmanned aerial vehicle firstly enters the height guiding section, tracks the sliding trajectory through the control method of the height guiding section, and carries out trajectory coarse adjustment during the whole landing process; the shipborne unmanned aerial vehicle enters the two-dimensional guiding section at the height of 200 m relative to the airport, and realizes accurate track of the trajectory through the control methodof the two-dimensional guiding section; and the shipborne unmanned aerial vehicle enters the tail end guiding section at the height of 15 m relative to the airport, and realizes that the nose of theunmanned aerial vehicle is aligned with the runway center line during landing of the unmanned aerial vehicle through the control method of the tail end guiding section. According to the autonomous control method for fixed point landing of shipboard unmanned aerial vehicle, the smooth transition of the shipboard unmanned aerial vehicle from the approach flat flying section to the sliding is realized; accurate track of the sliding trajectory line in the sliding process of the shipborne unmanned aerial vehicle is realized, the effect that the nose of the shipborne unmanned aerial vehicle is aligned with the runway center line during landing of the unmanned aerial vehicle is realized; and the precision of fixed point landing of the unmanned aerial vehicle is guaranteed.

Description

technical field [0001] The invention relates to the technical field of aviation flight control, in particular to an autonomous control method applied to fixed-point landing of a carrier-borne unmanned aerial vehicle. Background technique [0002] Compared with fixed-point landing of manned carrier-based aircraft, unmanned carrier-based aircraft has the advantages of high intelligence, safety and reliability, not limited by environmental factors, and no casualties. [0003] The land-based fixed-point landing test of the unmanned carrier-based aircraft not only ensures the safety of the carrier-based UAV system, but also provides technical reserves and support for the carrier-based UAV to intercept and land on the ship. Fixed-point landing is different from conventional landing. Conventional landing does not have high requirements on the accuracy of the landing point, and the UAV is controlled to "float" at a lower lifting speed when landing; while fixed-point landing has high...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05D1/10G05D1/08
CPCG05D1/0808G05D1/101
Inventor 邹阳魏林韩婵
Owner CHENGDU AIRCRAFT INDUSTRY GROUP
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