论文部分内容阅读
研究了近圆轨道上两个飞行器轨道交会的控制问题。通过对最优控制理论设计最优交会轨线的研究 ,提出了利用 H∞控制理论设计实际控制器的方法 ,给出了仿真结果 ,验证了这种方法的正确性。说明了该方法具有鲁棒的控制效果以及次优的轨道特性。
The control problem of the intersection of two aircraft orbits on a nearly circular orbit is studied. Based on the research on the optimal intersection trajectory of optimal control theory, a method of designing the actual controller based on H∞ control theory is proposed. The simulation results are given to verify the correctness of this method. It shows that this method has robust control effect and suboptimal orbit characteristics.