Indirect Control and Design of Insect-Like Flapping-Wing Micro Aerial Vehicle

Considering the Insect-like flapping-wing micro aerial vehicle, this paper has analyzed the composite of quasi-steady aerodynamics. That process has associated with the affection due to addition quality produced by wake capture. With introducing rotate circulation. This paper has calculated the lift, drag force, and pitch torque which take part on the wings' surfaces. Ignoring the wings' quality, the aircraft could be viewed as a rigid body. According to the Newton-Euler principle, establishing the dynamics model of aircraft is realized. And then, this paper has accomplished the indirect Adaptive controller and the update rate law. The algorithm could give dynamic compensation on uncertainty of the system. At last, this paper has taken the simulation of the algorithm. The result of that has verified the effectiveness of the controller design