rigid spacecraft dynamics

基本解釋

The dynamics of a rigid-liquid coupled spacecraft undergoing the encouragement of the pitching movement is investigated in the paper.
本文研究了充液貯箱在受到平面俯仰激勵時(shí)液體與貯箱的剛液耦合動力學(xué)問題。
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.
它分為多剛體系統(tǒng)動力學(xué)與多柔體系統(tǒng)動力學(xué)，有著很強(qiáng)的工程背景與實(shí)用價(jià)值，在航天器動力學(xué)與機(jī)器人動力學(xué)中有著廣泛地應(yīng)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.
研究一類構(gòu)形為中心剛性帶撓性梁的航天器平面快速大角度機(jī)動的動力學(xué)與控制問題。