Fault tolerant control of a quadrotor UAV using sliding mode control
Fault tolerant control of a quadrotor UAV using sliding mode control
- New search for: Sharifi, Farid
- New search for: Mirzaei, Mostafa
- New search for: Gordon, Brandon W.
- New search for: Zhang, Youmin
- New search for: Sharifi, Farid
- New search for: Mirzaei, Mostafa
- New search for: Gordon, Brandon W.
- New search for: Zhang, Youmin
In this paper, the sliding mode approach is used to control of a quadrotor UAV (Unmanned Aerial Vehicle) in the presence of external disturbance and actuator fault. Fault detection unit can detect the actuator fault using a state estimator. Then it reconfigures the structure of controller such that some control performance is achieved. The proposed control structure has the advantage of disturbance rejection in the fault-free condition. Moreover it can recover some of control performances when a fault occurs. Different simulations have been carried out to show the performance and effectiveness of the proposed method.
Document information
Fault tolerant control of a quadrotor UAV using sliding mode control
2010
6 Seiten, 9 Bilder, 18 Quellen
Conference paper
Storage medium
English
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