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A simple structure robust attitude synchronization with input saturation
Authors:Dong Ye  Yue Zhao  Jianxing Liu  Zhaowei Sun
Institution:1. Research Center of Satellite Technology, Harbin, 150001, PR China;2. Control theory and Engineering, School of Astronautics, Harbin Institute of Technology, Harbin, 150001, PR China;3. Research Institute of Intelligent Control and Systems, Harbin Institute of Technology, Harbin, 150001, PR China
Abstract:The attitude synchronization problem of multiple spacecraft is investigated in this paper. A simple cooperative control law, which can render spacecraft formation synchronized to a time-varying reference trajectory globally in the presence of model uncertainties, external disturbances and input saturation, is proposed. The globally asymptotic stability of the controller in the presence of model uncertainties and external disturbances is proven rigorously through a three-step proof technique. The controller can be used in orbit without modification due to its low computational complexity. Then, the proposed controller is extended to solve the consensus problem for multiple inertial agents with double-integrator dynamics. Finally, Numerical simulations are included to demonstrate the effectiveness of the developed controller.
Keywords:Corresponding author  
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