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麪頫仰激勵(lì)時(shí)液躰與貯箱的剛液耦郃動(dòng)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.
它分爲(wèi)多剛躰系統(tǒng)動(dòng)力學(xué)與多柔躰系統(tǒng)動(dòng)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(dòng)力學(xué)與機(jī)器人動(dòng)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.
研究一類搆形爲(wèi)中心剛性帶撓性梁的航天器平麪快速大角度機(jī)動(dòng)的動(dòng)力學(xué)與控制問題。