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Fault tolerant control of satellite formation flying using second order sliding mode control

机译:基于二阶滑模控制的卫星编队飞行容错控制

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摘要

Twisting, second order sliding mode control is presented to accommodate the thruster faults in the nonlinear MIMO picosatellite formation flying system with unknown time-varying disturbances. Robustness and stability of the proposed scheme is proved using twisting algorithm and its capability for formation keeping demonstrated against periodic thruster faults and external disturbances through simulations.
机译:提出了扭转二阶滑模控制,以适应未知时变扰动的非线性MIMO微小卫星编队飞行系统中的推进器故障。利用扭曲算法证明了该方案的鲁棒性和稳定性,并通过仿真证明了其对于周期性推进器故障和外部干扰的保持能力。

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