Abstract
This paper presents a path following controller for a quadrotor UAV experiencing a single rotor failure. A smooth, dynamic feedback control law is proposed that allows the quadrotor to follow both closed and non-closed embedded curves while maintaining a desired velocity profile along the path when one out of four motors is completely disabled due to failure. The nonlinear model of the quadrotor is transformed into a partially linear model by a coordinate and feedback transformation. A path following controller is designed for transformed system that guarantees invariance of the path. The uncontrolled nonlinear portion of the dynamics (internal dynamics) are shown to be bounded. © 2013 IEEE.
Original language | English (US) |
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Title of host publication | Proceedings of the IEEE Conference on Decision and Control |
Publisher | Institute of Electrical and Electronics Engineers Inc. |
Pages | 847-852 |
Number of pages | 6 |
ISBN (Print) | 9781467357173 |
DOIs | |
State | Published - Jan 1 2013 |
Externally published | Yes |