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Title:
ROCKET-BOOSTED LAUNCH AND TAKEOFF CONTROL METHOD FOR UNMANNED AERIAL VEHICLE HAVING FLYING-WING LAYOUT
Document Type and Number:
WIPO Patent Application WO/2023/240862
Kind Code:
A1
Abstract:
The present invention relates to the technical field of aviation flight control. Disclosed is a rocket-boosted launch and takeoff control method for an unmanned aerial vehicle having a flying-wing layout. The method is applicable to the control over a rocket-boosted launch and takeoff process of an unmanned aerial vehicle having a flying-wing layout. A control method that combines elevator pre-provision and pitch angle control is applied to a longitudinal controller, such that an aircraft is dynamically stable in the longitudinal direction at a launch and takeoff stage; roll angle control is applied to a transverse controller, such that wings are maintained flat, and after the aircraft climbs to a safety height, switching to flight trajectory tracking is performed; and a speed-based stability-augmentation softening factor is designed for a heading controller, such that an unmanned aerial vehicle is prevented from adverse disturbance caused by a rudder that is generated by low-speed angle-of-sideslip stability augmentation, and it is ensured that the unmanned aerial vehicle accesses stability augmentation control at a high-speed stage. The present invention is applicable to takeoff control over an unmanned aerial vehicle, which has a flying-wing layout and takes off on the basis rocket boosting.

Inventors:
LIU YUJIA (CN)
CUI QINGLIANG (CN)
ZHAO DONGHONG (CN)
ZHANG QUHUI (CN)
REN JIE (CN)
FANG XIONG (CN)
WANG ZHENDONG (CN)
WANG YI (CN)
TANG RUIQING (CN)
WANG QINGHU (CN)
Application Number:
PCT/CN2022/125685
Publication Date:
December 21, 2023
Filing Date:
October 17, 2022
Export Citation:
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Assignee:
CHENGDU AIRCRAFT IND GROUP CO LTD (CN)
International Classes:
G05D1/10
Foreign References:
CN114740902A2022-07-12
CN111309041A2020-06-19
CN110007683A2019-07-12
CN109634296A2019-04-16
US4721271A1988-01-26
Attorney, Agent or Firm:
CHENGDU JUNHEJI PATENT OFFICE (ORDINARY PARTNERSHIP) (CN)
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