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Nonlinear internal model based attitude tracking and disturbance rejection of rigid spacecraft

机译:基于非线性内模的刚性航天器姿态跟踪与干扰抑制

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In this paper, we consider the attitude tracking and disturbance rejection problem of rigid spacecraft subject to a class of nonharmonic periodic disturbances generated by nonlinear exosystems, which can not be handled by linear internal model. A nonlinear internal model is designed to deal with such disturbances. Numerical simulations illustrate the performance of the proposed control algorithms.
机译:在本文中,我们考虑了刚性飞船的姿态跟踪和扰动抑制问题,该问题会受到非线性外系统产生的一类非谐波周期性扰动的影响,而线性内部模型则无法解决这种扰动。设计了非线性内部模型来处理此类干扰。数值模拟说明了所提出的控制算法的性能。

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