The design of the high-precision attitude control system of the LEO
ISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics(2010)
摘要
This paper designs the H∞ state feedback controller of the low-orbit satellite to achieve the high precision attitude control. Based on the analysis of the system uncertainty and environment disturbance of the low-orbit satellite, H∞ method is adopted and the LMI arithmetic is used to make the computation easier. The results of the system simulation prove that the algorithm is useful and can make the attitude control system achieve the high precision requirements. ©2010 IEEE.
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关键词
attitude control,control systems,friction,satellites,flywheels,artificial satellites,uncertainty,state feedback controller
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