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摘要
Attitude stabilization and tracking is an important issue in the flight of the Quadrotor, especially in the windy environment. This paper focus on the attitude stabilization and tracking problem, detailed mathematical modeling was proposed and two kinds of attitude control architectures were evaluated through mathematical simulations, meanwhile the zero-mean white noise was added to the control signal, the simulation results verify the feasibility of the proposed control laws.
- 出版日期2016
- 单位西安工业大学
