Complex attitude adaptive control method after multi-rotor aircraft captures target
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- 上海铸天智能科技有限公司
- Publication Date
- 2017-04-19
- Estimated Expiration
- Not applicable · inactive patent
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Abstract
Description
technical field
[0001] The invention relates to the technical field of multi-rotor aircraft control, in particular to a complex attitude adaptive control method after the multi-rotor aircraft captures a target. Background technique
[0002] Unlike traditional single-rotor helicopters, the unique symmetrical layout of multi-rotor aircraft does not need to change the pitch to provide the main lift and torque required in flight, so that it can quickly switch between position movement and hovering at any time; except In addition, its small-sized propeller design greatly improves the stealth of flight and the safety of flight in unknown environment. Therefore, in recent years, multi-rotor aircraft has attracted extensive attention from domestic and foreign scholars and scientific research institutions due to its unique flight stability, simple structure, easy control and high safety performance, and has quickly become one of the current international research hotspots. . [000...