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Sensor fault-tolerant observer applied in satellite attitude control 被引量:2
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作者 Jiaolong Wei zhaohui cen Rui Jiang 《Journal of Systems Engineering and Electronics》 SCIE EI CSCD 2012年第1期99-107,共9页
The observing failure and feedback instability might happen when the partial sensors of a satellite attitude control sys- tem (SACS) go wrong. A fault diagnosis and isolation (FDI) method based on a fault observer... The observing failure and feedback instability might happen when the partial sensors of a satellite attitude control sys- tem (SACS) go wrong. A fault diagnosis and isolation (FDI) method based on a fault observer is introduced to detect and isolate the fault sensor at first. Based on the FDI result, the object system state-space equation is transformed and divided into a correspon- sive triangular canonical form to decouple the normal subsystem from the fault subsystem. And then the KX fault-tolerant observers of the system in different modes are designed and embedded into online monitoring. The outputs of all KX fault-tolerant observers are selected by the control switch process. That can make sense that the SACS is part-observed and in stable when the partial sen- sors break down. Simulation results demonstrate the effectiveness and superiority of the proposed method. 展开更多
关键词 triangular canonical form KX observer satellite atti- tude control integrity in closed-loop
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