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A model-based solution for fault diagnosis of thruster faults: application to the rendezvous phase of the mars sample return mission
2013
Progress in Flight Dynamics, Guidance, Navigation, Control, Fault Detection, and Avionics
unpublished
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This paper addresses the design of model-based fault diagnosis schemes to detect and isolate faults occurring in the orbiter thrusters of the Mars Sample Return (MSR) mission. The proposed fault diagnosis method is based on a H(0) ¦lter with robust poles assignment to detect quickly any kind of thruster faults and a cross-correlation test to isolate them. Simulation results from the MSR ¤high-¦delity¥ nonlinear simulator provided by Thales Alenia Space demonstrate that the proposed method is
doi:10.1051/eucass/201306423
fatcat:skfgvz5gzrdbnncxwmvz26vy4u