Nonlinear control of quadrotor UAV under rotor failure for robust trajectory tracking

Abstract We present a trajectory tracking control law for a quadrotor unmanned aerial vehicle (UAV) for handling the complete failure of a single rotor. The control design problem considers the reduced state space, which excludes the angular velocity and orientation about the vertical body axis. The...

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Номзүйн дэлгэрэнгүй

Үндсэн зохиолчид:	Ashutosh Simha, Leszek Ambroziak
Формат:	Artigo
Хэл сонгох:	Inglês
Хэвлэсэн:	Nature Portfolio 2025-11-01
Цуврал:	Scientific Reports
Нөхцлүүд:	Nonlinear control Geometric control Reduced attitude tracking Rotor failure Quadrotor
Онлайн хандалт:	https://doi.org/10.1038/s41598-025-26264-x
Шошгууд:	Шошго нэмэх Шошго байхгүй, Энэхүү баримтыг шошголох эхний хүн болох!