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In this paper, in the case of complete propeller motor failures, a feedback-loop control for a multirotor to avoid a crash when some motors fail and stop, is presented, and verified by simulation results. First, the modeling foundation for a multirotor, and the flight states are summarized. Secondly, theorems of the stabilizability of the flight states for avoiding a crash, by nonlinear dynamic state equations with state variable feedbacks are provided, andalso verified by simulations. In conclusion, the principal results are summarized, and the future research is described.
Hexarotor Motor Failure Problem Stable Flights To Avoid a Crash
Hexarotor Motor Failure Problem Stable Flights To Avoid a Crash
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