摘要：AbstractAn integration of Fault Detection, Isolation and Recovery (FDIR) with the Linear Quadratic Gaussian (LQG) technique is presented, which achieves fault tolerance while maintaining control optimality. The FDIR scheme is tested on a space micro-launcher model, and simulation results show successful accommodation of both sensor and actuator faults.
关键词：KeywordsAerospace controlLQG controlFault detectionFault diagnosisFault tolerant systems
