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FORMATION FLIGHT SYSTEM VIA ROBUST CONTROL

机译:通过强大的控制形成飞行系统

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摘要

Clohessy-Wiltshire (C-W) Equation has been widely used to model the leader-follower dynamics for the formation flight system. Numerous controllers have been proposed based on this linear model. To date, most of these controllers assumed that the system model is well defined, and all the states are known. However, since the C-W equation is only a linear approximation of the physical system and is restricted to the near circular reference orbit, in this paper, LQR and H_∞ / μ controllers are designed based on this linear C-W model with robustness against parametric uncertainty and the un-modeled high order dynamics. These linear robust controllers are evaluated in simulation using both linear and nonlinear models. The simulation results demonstrate that LQR and H_∞ / μ controllers are capable of controlling the nonlinear model.
机译:CLOHESSY-WILTSHIRE(C-W)方程已被广泛用于模拟地层飞行系统的领导者动态。基于该线性模型提出了许多控制器。迄今为止,大多数这些控制器都假定系统模型定义很好,并且所有状态都是已知的。然而,由于CW等式仅是物理系统的线性近似,并且仅限于近圆形参考轨道,本文基于该线性CW模型设计了LQR和H_∞/μ控制器,该模型具有针对参数不确定性的鲁棒性和未建模的高阶动态。使用线性和非线性模型在仿真中进行评估这些线性鲁棒控制器。仿真结果表明,LQR和H_∞/μ控制器能够控制非线性模型。

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