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A velocity-free attitude tracking controller for rigid spacecraft

机译:刚性航天器的无速度姿态跟踪控制器

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In this paper, we propose a quaternion-based dynamic output feedback for the attitude tracking problem of a rigid body without velocity measurement. Our approach consists of introducing an auxiliary dynamical system whose output (which is also a unit quaternion) is used in the control law together with the unit quaternion representing the attitude tracking error. Roughly speaking, the necessary damping that would have been achieved by the direct use of the angular velocity can be achieved, in our approach, by the vector part q of the error signal between the output of the auxiliary system and the unit quaternion tracking error. The resulting velocity-free control scheme guarantees almost global asymptotic stability which is as strong as the topology of the motion space can permit. Simulation results are provided to show the effectiveness of the proposed control scheme.
机译:在本文中,我们提出了一种基于四元的动态输出反馈,用于刚体的姿态跟踪问题而没有速度测量。我们的方法包括引入辅助动态系统,其输出(即单位四元数)与表示姿态跟踪误差的单位四元数一起使用。粗略地说,通过直接使用角速度来实现的必要阻尼,通过辅助系统的输出和单位四元线跟踪误差之间的误差信号的误差信号的矢量部分Q可以实现。由此产生的速度控制方案既保证了几乎全局渐近稳定性,就像运动空间的拓扑可以允许的那样强有力。提供了仿真结果以表明所提出的控制方案的有效性。

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