Miniature double-flapping-wing aircraft capable of realizing autonomous stability augmentation control and control moment generation method thereof
Patent Information
- Authority / Receiving Office
- CN · China
- Current Assignee / Owner
- BEIHANG UNIV
- Publication Date
- 2021-02-02
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Abstract
Description
technical field
[0001] The invention relates to the field of micro-aircraft, in particular to a miniature double-flapping-wing aircraft capable of autonomous stability enhancement control and a method for generating control torque thereof. Background technique
[0002] With the continuous innovation of aircraft design concepts and the great progress of microelectronics technology at the end of the last century, micro air vehicles were proposed and developed rapidly. With the characteristics of small size, light weight and strong maneuverability, micro air vehicles are suitable for reconnaissance, exploration and rescue assistance in complex environments, and have broad application prospects. As an important branch of micro-aircraft, the bionic flapping-wing micro-aircraft gradually began to appear with the development of bionics design. The flapping-wing micro-aircraft relies on the reciprocating flapping of the flapping wings to generate lift, and generates control torque ...