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Extension of a PID control theory to Lie groups applied to synchronising satellites and drones

机译:扩展PID控制理论,撒谎组应用于同步卫星和无人机

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摘要

The authors tackle time synchronisation of two (possibly non-identical) second-order dynamical systems whose state space possess the structure of a Lie group. Synchronisation is treated as a non-linear control problem on Lie groups. They present a control theory inspired by the proportional–integral–derivative (PID) regulation principle. The resulting L-PID control scheme is applied to sync the rotational component of motions in physical systems. A model-dependent version of the L-PID, equipped with a dynamics-cancelling component, is theoretically proven to converge to zero control error by a Lyapunov stability analysis. Furthermore, they present Lie-group-tailored numerical techniques to implement the devised PID regulation theory and test such numerical schemes on two dynamical systems, namely, a gyrostat satellite and a quadrotor drone. As a further extension, they present an empirical translational synchronisation algorithm for two drones based on a pair of concurring L-PID and projected-PID controllers.
机译:作者提出了两个(可能是非相同)二阶动态系统的时间同步,其状态空间具有LIE组的结构。同步被视为LIE组上的非线性控制问题。他们提出了一种受到比例 - 积分衍生物(PID)调节原理的控制理论。应用了L-PID控制方案以在物理系统中同步运动的旋转分量。通过Lyapunov稳定性分析,理论上证明,配备有动力取消组件的L-PID的模型依赖版本,以通过Lyapunov稳定性分析来收敛到零控制误差。此外,它们呈现Lie-Group-Treatored数值技术,以实现设计的PID调节理论,并在两个动态系统上测试这种数值方案,即Gyrostat卫星和四足芳车无人机。作为另一个扩展,它们基于一对同时的L-PID和投影 - PID控制器呈现了两个无人机的经验翻译同步算法。

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