挠性航天器快速机动输出反馈控制 - 中南大学学报（自然科学版、英文版） 关键字: 挠性航天器；快速机动；输出反馈；无源性[gap=656]Key words: flexible spacecraft; fast maneuver; output feedback; passivity
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nonlinear flexible spacecraft 非线性挠曲宇宙飞船
flexible spacecraft dynamics [航] 挠性航天器动力学
large flexible spacecraft attitude control 大型挠性航天器的姿态控制
large flexible spacecraft vibration control 大型挠性航天器的振动控制
Flexible liquid spacecraft 挠性充液航天器
Flexible Multibody Spacecraft 挠性多体航天器
Numerical simulation results of an application to flexible spacecraft are also presented to verify the effectiveness of the control law derived here.
最后将所提出的方法应用于某型挠性航天器的姿态稳定任务中,仿真结果验证了该方法的有效性。
参考来源 - 执行器故障的挠性航天器姿态滑模容错控制Based on Lagrange's method, the flexible spacecraft with a rigid center hub and two identical flexible appendages is modeled. And the model is simplified for control.
针对“一个中心刚体+两个对称安装的太阳帆板”的挠性航天器，用Lagrange方法建立了系统的动力学模型，并在此基础上给出了用于设计控制规律的简化模型。
参考来源 - 建立大柔性多体结构航天器的动力学模型与面向控制的仿真平台·2,447,543篇论文数据，部分数据来源于NoteExpress
The dynamic equations of flexible spacecraft are derived by introducing a moving coordinate frame.
首先建立了采用任意浮动参考系时的柔性航天器动力学方程；
The problem of robust attitude control for three-axial-stabilized flexible spacecraft is considered.
研究三轴稳定的挠性航天器姿态的鲁棒控制问题。
Finally, it is considered that the stability of flexible spacecraft with liquid-filled multi-body system.
最后，讨论了多体系统充液挠性空间飞行器的稳定性问题。
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