Abstract
A failure detection, identification and reconfiguration (FDIR) control scheme is developed for a dynamic model of the delta clipper-experimental (DC-X) single stage to orbit rocket concept. The six degree of freedom, redundantly actuated model provides a well-suited test case for designing a fault-tolerant controller for actuators with different response rates, the reconfigurable controller maintains the desired closed-loop performance. Robustness of the system was demonstrated under a large number of different single and multiple failure cases.
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