In this paper, we propose a strategy for detecting and isolating actuator faults in an overactuated Remotely Operated Vehicle (ROV) with six degrees of freedom. Fault detection and isolation are based on the Adaptive Extended Kalman Filter (AEKF), which is a recent extension of the well-known Kalman Filter designed for nonlinear dynamics and additive disturbances estimation. The residuals generated by the AEKF act as directional residuals, and fault isolation is performed by calculating the cosine similarity between the residuals and the columns of the control effectiveness matrix. The decision is then used in a simple fault-tolerant control allocation algorithm, without the need to alter the control law. Simulation results show the effectiveness of the estimation method in the presence of thruster failures.

Actuator Fault Tolerant Control for a Remotely Operated Vehicle based on Adaptive Extended Kalman Filter / Baldini, Alessandro; Felicetti, Riccardo; Freddi, Alessandro; Monteriu', Andrea. - 58:(2024), pp. 61-66. (Intervento presentato al convegno 12th IFAC Symposium on Fault Detection, Supervision and Safety for Technical Processes, SAFEPROCESS 2024 tenutosi a Ferrara, Italia nel 4-7 giugno 2024) [10.1016/j.ifacol.2024.07.194].

Actuator Fault Tolerant Control for a Remotely Operated Vehicle based on Adaptive Extended Kalman Filter

Baldini Alessandro
Primo
;
Felicetti Riccardo
Secondo
;
Freddi Alessandro
Penultimo
;
Monteriu' Andrea
Ultimo
2024-01-01

Abstract

In this paper, we propose a strategy for detecting and isolating actuator faults in an overactuated Remotely Operated Vehicle (ROV) with six degrees of freedom. Fault detection and isolation are based on the Adaptive Extended Kalman Filter (AEKF), which is a recent extension of the well-known Kalman Filter designed for nonlinear dynamics and additive disturbances estimation. The residuals generated by the AEKF act as directional residuals, and fault isolation is performed by calculating the cosine similarity between the residuals and the columns of the control effectiveness matrix. The decision is then used in a simple fault-tolerant control allocation algorithm, without the need to alter the control law. Simulation results show the effectiveness of the estimation method in the presence of thruster failures.
2024
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11566/337060
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