Abstract
An integrated design of fault diagnosis and reconfiguration method is studied for actuator failures of satellite control system. First, the effectiveness factor and the controller gain are taken as a whole to design the combined control law, which is obtained by placing the closed-loop system poles according to the theory of regional pole assignment. And this paper uses perturbation linearization method to solve the generating bilinear matrix inequalities(BMI). Then the effectiveness factor is obtained with a two-stage Kalman filter and thus the control law can be solved. Finally, the effectiveness of the provided method is illustrated by a simulation.
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Liu, X., Liu, C. (2016). Integrated Design of Fault Diagnosis and Reconfiguration for Satellite Control System. In: Jia, Y., Du, J., Zhang, W., Li, H. (eds) Proceedings of 2016 Chinese Intelligent Systems Conference. CISC 2016. Lecture Notes in Electrical Engineering, vol 405. Springer, Singapore. https://doi.org/10.1007/978-981-10-2335-4_44
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DOI: https://doi.org/10.1007/978-981-10-2335-4_44
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