太阳帆航天器姿态动力学建模与反馈线性参数变化控制

Attitude Dynamic Modeling and Feedback LPV Control of Solar Sail

  • 摘要: 针对太阳帆航天器的薄膜帆面和大尺度杆的柔性特征,建立了太阳帆航天器非线性刚柔耦合动力学模型.在满足一定假设条件时,该模型可以转化为多胞线性参数变化(LPV)系统.针对该多胞LPV系统设计了一种状态反馈控制律,通过求解带线性参数不等式约束的凸优化问题,得到了控制器参数的解.仿真结果表明,所提的控制算法既实现了太阳帆目标姿态角的渐近跟踪,又实现了柔性结构的振动抑制.

     

    Abstract: In consideration of the extreme flexibility characteristics of film sail and large-scale booms of solar sail, a nonlinear rigid-flexible coupling dynamic model is presented. Under some assumptions, the model is translated into a polytopic linear parameter-varying (LPV) system, and then a state feedback control law is designed for the polytopic LPV system. Solutions of the parameters of the controller are obtained by solving the convex optimization problem with linear matrix inequality (LMI) constraints. Finally the simulation results show that the proposed method is effective, as the asymptotic tracking of the sail target attitude angle and robust vibration suppression of flexible structures are all achieved.

     

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