Robust Control Technigue of Flexible Satellite Attitude Movement
- 航空航天－已发表论文 
具有挠性振动和液体晃动的新一代挠性卫星姿态运动是一个不确定系统 ,运用 H∞ 优化与 μ综合技术研究具有抑制振动和晃动能力以及强鲁棒性的卫星姿态控制系统设计问题 ,并对所提出的几种鲁棒控制系统设计方案进行计算机仿真和全物理仿真实验研究 .Attitude movement of new style flexible satellite is uncertain systems. The control system design problem with the suppession of the flexible structure vibration and the liquid sloshing as well as the strong robustness was studied by using H ∞ optimal method and μ synthesis technigue. The computer simulation and physical simulation experiment were also studied for some robust control schemes.