机译:输入饱和和测量不确定性的基于扰动观测器的航天器鲁棒后推姿态稳定
Seventh Research Division, Science and Technology on Aircraft Control Laboratory, School of Automation Science and Electrical Engineering, Beihang University, School of Automation and Electrical Engineering, University of Science and Technology Beijing, Beijing, Beijing, ChinaChina;
Seventh Research Division, Science and Technology on Aircraft Control Laboratory, School of Automation Science and Electrical Engineering, Beihang University, Beijing, China;
Attitude control; Measurement uncertainty; Space vehicles; Observers; Uncertainty; Robustness; Backstepping;
机译:受致动器饱和影响的挠性航天器的鲁棒自适应反推姿态稳定和减振
机译:输入饱和下基于扰动观测器的鲁棒相对姿态控制用于航天器交会和近距操作
机译:输入饱和下航天器姿态跟踪的反推控制
机译:具有输入饱和度和参数不确定性的航天器悬停的自适应反步控制
机译:测试土壤碳饱和度理论:最大碳稳定度和土壤有机质稳定性随有机碳输入的变化而变化。
机译:具有执行器动力学的航天器航天器的有限时间态度稳定控制
机译:致动器故障和不确定性下航天器姿态稳定的鲁棒控制分配