rigid spacecraft dynamics

基本解释

The dynamics of a rigid-liquid coupled spacecraft undergoing the encouragement of the pitching movement is investigated in the paper.
本文研究了充液贮箱在受到平面俯仰激励时液体与贮箱的刚液耦合动力学问题。
It contains rigid bodies dynamics and flexible multibody system dynamics. It has great of practice values. It is greatly applied in Robotics and Spacecraft dynamics.
它分为多刚体系统动力学与多柔体系统动力学，有着很强的工程背景与实用价值，在航天器动力学与机器人动力学中有着广泛地应用。
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。