This paper investigates the robust control of large Angle maneuver for the multi-body spacecraft with model uncertainties.
研究了具有模型不确定性的多体航天器大角度机动控制问题。
The recently developed nonlinear active disturbance rejection controller (ADRC) is applied to attitude control of large flexible multi-body satellite with reaction wheels.
研究了最近提出的非线性自抗扰控制器(adrc)在大挠性多体卫星姿态控制中的应用问题。
The recently developed nonlinear Active Disturbance Rejection Controller (ADRC) was applied to the attitude control of large flexible multi-body satellite with reaction wheels.
研究了最近提出的非线性自抗扰控制器在大挠性多体卫星姿态控制中的应用问题。
This paper is concerned with the dynamics and control for planar, large Angle rapid slew maneuvering of a flexible multi body spacecraft, consisting of a rigid central body and a flexible beam.
研究一类构形为中心刚性带挠性梁的航天器平面快速大角度机动的动力学与控制问题。
Using the advantage of centralized control and multi-agent plan theory, a framework model including one control coordinate intellectual body and 3 plan carry out intellectual body was build up.
利用集中控制的优点和多智能体规划理论，设计了包括一个控制协调智能体和3个计划执行智能体在内的结构模型。
Using the advantage of centralized control and multi-agent plan theory, a framework model including one control coordinate intellectual body and 3 plan carry out intellectual body was build up.
利用集中控制的优点和多智能体规划理论，设计了包括一个控制协调智能体和3个计划执行智能体在内的结构模型。
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