[1]毕显婷,史小平.带有输入时延的刚性航天器反最优姿态控制[J].电机与控制学报,2017,21(03):83-88.[doi:10.15938/j. emc.2017.03.012] BI Xian-ting,SHI Xiao-ping. Inverse optimal stabilization of ri^;id spacecraft in presence of input delay[J].,2017,21(03):83-88.[doi:10.15938/j. emc.2017.03.012]
An attitude stabilization controller of the rigid spacecraft in the presence of input delay was proposed. Firstly,a Lyapunov function was constructed after backstepping transformation of the original spacecraft model,and a time delay compensated controller that can guarantee global asymptotic stability was obtained. Considering the strong coupling nonlinearity of spacecraft system,the inverse optimal theory was then utilized to construct a cost functional with penalty on both system states and control torque, which reflects the importance of energy cost,and the optimal controller was consequently obtained. Compared withi the optimal controller,the controller without optimal consideration costs more energy,quantitative analysis was given in simulation.Simulation results show the proposed controller is effective In attitude stabilization with different time delay,moreover,it is robust with delay uncertainty.
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