Trajectory Tracking Control of a Quadrotor Unmanned Mini-Helicopter
نویسندگان
چکیده
In this paper, the relationship between attitude and linear acceleration of the quadrotor unmanned mini-helicopter is built and two trajectory tracking control design methodologies based on the relationship are proposed: classical inner/outer-loop control design approach and a new command filtered backstepping design strategy. Various numerical simulations demonstrate the validity of the control design. Finally, we discuss the two design methods and arrive at a conclusion via comparison.
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