This paper presents an attitude and altitude fault-tolerant tracking control for a quadrotor using the Disturbance Observer Based Control (DOBC). A Newton-Euler model of the quadrotor is described and the fault-tolerant control problem is treated for small angles. An appropriate estimation gain is proposed for the considered system, which allows to impose desired closed loop performances. These closed loop performances are analysed, showing the boundedness properties, and highlighting the trade off between fault estimation and control effort. Numerical simulations are provided for testing the effectiveness of the proposed DOBC solution, which is compared with the classical backstepping controller in case of multiple actuation faults.
Fault-Tolerant Disturbance Observer Based Control for Altitude and Attitude Tracking of a Quadrotor / Baldini, Alessandro; Felicetti, Riccardo; Freddi, Alessandro; Longhi, Sauro; Monteriu, Andrea. - ELETTRONICO. - (2018), pp. 685-690. (Intervento presentato al convegno 26th Mediterranean Conference on Control and Automation, MED 2018 tenutosi a hrv nel 2018) [10.1109/MED.2018.8443048].
Fault-Tolerant Disturbance Observer Based Control for Altitude and Attitude Tracking of a Quadrotor
Baldini, Alessandro;Felicetti, Riccardo;Freddi, Alessandro;Longhi, Sauro;Monteriu, Andrea
2018-01-01
Abstract
This paper presents an attitude and altitude fault-tolerant tracking control for a quadrotor using the Disturbance Observer Based Control (DOBC). A Newton-Euler model of the quadrotor is described and the fault-tolerant control problem is treated for small angles. An appropriate estimation gain is proposed for the considered system, which allows to impose desired closed loop performances. These closed loop performances are analysed, showing the boundedness properties, and highlighting the trade off between fault estimation and control effort. Numerical simulations are provided for testing the effectiveness of the proposed DOBC solution, which is compared with the classical backstepping controller in case of multiple actuation faults.I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.