考虑转矩饱和的有限时间容错航天器姿态控制

Q. Hu, Xiao Tan, M. Akella
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引用次数: 43

摘要

针对由推力驱动的刚性航天器,提出了一种平滑姿态稳定控制器,该控制器在存在外部干扰、输入饱和和惯性条件下均能实现有限时间稳定。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Finite-Time Fault-Tolerant Spacecraft Attitude Control with Torque Saturation
A smooth attitude-stabilizing controller is proposed for rigid spacecraft actuated by thrusters that achieves finite-time stability in the presence of external disturbance, input saturation, and in...
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