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Patent Searching and Data


Title:
FLIGHT CONTROL METHOD AND RELATED APPARATUS
Document Type and Number:
WIPO Patent Application WO/2021/037071
Kind Code:
A1
Abstract:
A flight control method and related apparatus, which can determine different detour flight lines according to position information of obstacles in different ranges, and the end point of the determined detour flight line may also vary with the position information of obstacles in different ranges, thereby enabling an unmanned aerial vehicle (100) to flexibly bypass obstacles in different ranges, so that in complex operation scenarios, the unmanned aerial vehicle (100) automatically and efficiently bypasses obstacles. The method comprises: when position information of an obstacle is within a detour range of a cross flight segment, generating a detour flight line of the cross flight segment according to the position information of the obstacle, so that the unmanned aerial vehicle (100) detours along the detour flight line of the cross flight segment to a starting safety point of the next flight segment (S130); and when the position information of the obstacle is within a detour range of a present flight segment, generating a detour flight line of the current flight segment according to the position information of the obstacle, so that the unmanned aerial vehicle (100) detours along the detour flight line of the current flight segment to a starting safety point of the current flight segment (S140).

Inventors:
ZHENG LIQIANG (CN)
Application Number:
PCT/CN2020/111436
Publication Date:
March 04, 2021
Filing Date:
August 26, 2020
Export Citation:
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Assignee:
GUANGZHOU XAIRCRAFT TECH CO LTD (CN)
International Classes:
G05D1/10
Foreign References:
CN109947123A2019-06-28
CN107883962A2018-04-06
CN104359473A2015-02-18
CN106843260A2017-06-13
CN104807457A2015-07-29
CN104503463A2015-04-08
CN109062259A2018-12-21
CN107340781A2017-11-10
CN103218660A2013-07-24
US20150066248A12015-03-05
Attorney, Agent or Firm:
CHOFN INTELLECTUAL PROPERTY (CN)
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