A multi-objective parametric design method that based on the robust observer is proposed for the attitude control of satellites with super flexible netted antennas. First, a parametric observer-based controller is obtained based on the eigen-structure assignment theory. The closed-loop poles are assigned to desired positions or regions, and full degrees of freedom of the design, which are characterized by a set of parameters, are preserved under the proposed control law. Second, the obtained parameters are comprehensively optimized to make the closed-loop system have lower eigenvalue sensitivity, a smaller control gain, and stronger tolerance to high-order unmodeled dynamics and external disturbances. Finally, comparative simulations are carried out based on practical engineering parameters of a satellite in order to verify the effect of the proposed method, and also to show their superiority over the traditional proportional-integral-derivative (PID) controller with filters and the traditional dynamic compensators.

提出了一种基于鲁棒观测器的多目标参数化设计方法，用于超柔性网状天线的卫星姿态控制。首先，基于特征结构分配理论，获得了基于参数观测器的控制器。将闭环极点分配给所需的位置或区域，并根据建议的控制法则保留以一组参数为特征的设计的完整自由度。其次，对获得的参数进行全面优化，以使闭环系统具有较低的特征值灵敏度，较小的控制增益以及对高阶非模型动力学和外部干扰的较强耐受性。最后，