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Aircraft landing method and auxiliary device

A technology for an auxiliary device and an aircraft, applied in the field of information processing, can solve problems such as hidden safety hazards, labor costs, difficulty in accurate landing guidance, and restrictions on the wide-area and large-scale deployment of aircraft systems, so as to reduce operational burden and improve landing safety.

Inactive Publication Date: 2017-11-28
BEIHANG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

This method has lower requirements on the intelligent degree and precise situational awareness of the flight control system, and mainly relies on the operational level and experience of the ground operators, and the landing guidance is difficult to be accurate.
Since the core feature of semi-autonomous landing is human control, it leads to obvious safety hazards and labor costs, which limits the ability of the aircraft system to be deployed in a wide area.

Method used

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  • Aircraft landing method and auxiliary device
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  • Aircraft landing method and auxiliary device

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Embodiment Construction

[0037] In order to make the purpose, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments It is a part of embodiments of the present invention, but not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention.

[0038] The technical solution of the present invention will be described in detail below with specific embodiments. The following specific embodiments may be combined with each other, and the same or similar concepts or processes may not be repeated in some embodiments.

[0039] figure 1 It is a flow chart of the aircraft landing method in Embod...

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PUM

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Abstract

The embodiment of the invention relates to the field of information processing, in particular to an aircraft landing method and an auxiliary device. The aircraft landing method comprises the steps that an aircraft receives a landing instruction; the aircraft detects a landing identification within the preset range, and the landing identification comprises two-dimensional codes, and the two-dimensional codes carry landing information; the aircraft identifies the two-dimensional codes and obtains the landing information; the aircraft executes the landing action according to the landing information. According to the aircraft landing method and the auxiliary device, close-distance space relative position determining can be achieved without a positioning system, full-autonomous precise landing of the aircraft can be achieved, operation burdens of an operator can be effectively reduced, and the landing safety of the aircraft is improved.

Description

technical field [0001] Embodiments of the present invention relate to the field of information processing, and in particular to an aircraft landing method and an auxiliary device. Background technique [0002] Aircraft can be divided into manned and unmanned, both of which are widely used in various fields. Among various types of aircraft systems, aircraft with vertical take-off and landing capabilities play an important role due to their flexible take-off and landing and convenient deployment. Mission capability and application value. [0003] In the prior art, semi-autonomous landing methods are widely used for aircraft with vertical take-off and landing capabilities, in which the airborne flight control system controls the flight platform to move over the target landing area, and then the ground operators generally determine the landing position and perform the landing attitude fine-tuning. This method has lower requirements on the intelligence and precise situational a...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D45/04G05D1/08G06K17/00
CPCB64D45/04G05D1/0808G06K17/00
Inventor 谢晋东肖振宇尹超
Owner BEIHANG UNIV
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