Title :
Integrated active fault-tolerant control using IMM approach
Author :
Zhang, Youmin ; Jiang, Jin
Author_Institution :
Dept. of Electr. & Comput. Eng., Univ. of Western Ontario, London, Ont., Canada
fDate :
10/1/2001 12:00:00 AM
Abstract :
An integrated fault detection, diagnosis, and reconfigurable control scheme based on interacting multiple model (IMM) approach is proposed. Fault detection and diagnosis (FDD) is carried out using an IMM estimator. An eigenstructure assignment (EA) technique is used for reconfigurable feedback control law design. To achieve steady-state tracking, reconfigurable feedforward controllers are also synthesized using input weighting approach. The developed scheme can deal with not only actuator and sensor faults, but also failures in, system components. To achieve fast and reliable fault detection, diagnosis, and controller reconfiguration, new fault diagnosis and controller reconfiguration mechanisms have been developed by a suitable combination of the information provided by the mode probabilities from the IMM algorithm and an index related to the closed-loop system performance. The proposed approach is evaluated using an aircraft example, and excellent results have been obtained
Keywords :
adaptive control; aircraft control; closed loop systems; control system synthesis; eigenstructure assignment; fault diagnosis; fault tolerance; feedforward; hidden Markov models; linear quadratic control; probability; robust control; state estimation; state feedback; Kalman filter; LQR-based control design; actuator faults; aircraft fault detection; closed-loop system performance; closed-loop system stability; eigenstructure assignment; fast reliable fault detection; fault detection and diagnosis; finite-state Markov chain; input weighting approach; integrated active fault-tolerant control; interacting multiple model approach; mode probabilities; reconfigurable feedback control law design; reconfigurable feedforward controllers; robustness; sensor faults; state estimation; steady-state tracking; Actuators; Control system synthesis; Control systems; Fault detection; Fault diagnosis; Fault tolerance; Feedback control; Sensor systems; Steady-state; System performance;
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on