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Attitude Sampling Tracking Control For A Rigid Spacecraft Via Backstepping

机译:通过BackStepping将刚性宇宙飞船的姿态采样跟踪控制

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This paper is concerned with the issue of attitude tracking control design for a rigid spacecraft. We first transform the attitude dynamics into a strict-feedback system by using a change of coordinates. And then, based on a continuous-time controller designed by using Backstepping technique, a multi-rate sampled-data controller is proposed to achieve the asymptotic stability of the closed-loop system. The effectiveness of the proposed approach is verified through a numerical example.
机译:本文涉及刚性航天器的态度跟踪控制设计问题。我们首先使用坐标的变化将态度动态转换为严格反馈系统。然后,基于通过使用反向技术技术设计的连续时间控制器,提出了一种多速率采样数据控制器来实现闭环系统的渐近稳定性。通过数值示例验证了所提出的方法的有效性。

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