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Globally Stabilizing Proportional-Integral-Derivative Control Laws for Rigid-Body Attitude Tracking

机译:用于刚体姿态跟踪的全球稳定比例-积分-微分控制法

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摘要

Attitude control of a rigid body has important applications to aircraft and spacecraft. Various control laws have been developed for pointing and slewing [1-17]. To enhance the flight envelope of a spacecraft system, globally stabilizing control laws are widely desired for attitude control. In attitude control of a rigid-body, singular orientation and the unwinding phenomenon are two major obstacles to designing a globally stabilizing control law [1].
机译:刚体的姿态控制在飞机和航天器中具有重要的应用。已经开发了各种用于定点和回转的控制定律[1-17]。为了增强航天器系统的飞行包线,高度稳定的控制律被广泛地要求用于姿态控制。在刚体的姿态控制中,奇异的方向和展开现象是设计全局稳定控制律的两个主要障碍[1]。

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  • 来源
    《Journal of guidance, control, and dynamics》 |2011年第4期|p.1260-1264|共5页
  • 作者

    Jingya Su; Kai-Yuan Cai;

  • 作者单位

    Beijing University of Aeronautics and Astronautics, 100191 Beijing, People's Republic of China School of Automation Science and Electrical Engineering, National Key Laboratory of Science and Technology on Holistic Control;

    Beijing University of Aeronautics and Astronautics, 100191 Beijing, People's Republic of China School of Automation Science and Electrical Engineering, National Key Laboratory of Science and Technology on Holistic Control;

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