A new attitude maneuver using kinematics and dynamics of non-holonomic turn

研究成果: Conference contribution

1 被引用数 (Scopus)

抄録

This paper shows the dynamic properties interpreted about a falling cat motion. A new interpretation on non-holonomic turns was presented from coning effect point of view. It infers even the kinematics effect independent of dynamics may still drive the non-holonomic turn. However, that motion is, in this paper, proved not fully true and shown partly dependent on the inertia properties. This paper presents new interpretation findings which show the resulted non-holonomic turn may become reverse dependent on the moment of inertia ratio. This paper corrects the motion structure interpretation, in which a very interesting combination of kinematics and dynamics is found to govern the motion. And a numerical example is given for the spacecraft attitude maneuver, whose time history is explicitly described. A special feedforward control law is derived and applied to the maneuver. The results show the control strategy established well functions and enables the reorientation to be accomplished only via internal torque. What is presented does provide a comprehensive strategy widely applicable to spacecraft and space robots.

本文言語English
ホスト出版物のタイトルSpaceflight Mechanics 2006 - Proceedings of the AAS/AIAA Space Flight Mechnaics Meeting
ページ3-15
ページ数13
出版ステータスPublished - 2006
外部発表はい
イベントSpaceflight Mechanics 2006 - AAS/AIAA Space Flight Mechnaics Meeting - Tampa, FL, United States
継続期間: 2006 1 222006 1 26

出版物シリーズ

名前Advances in the Astronautical Sciences
124 I
ISSN(印刷版)0065-3438

Conference

ConferenceSpaceflight Mechanics 2006 - AAS/AIAA Space Flight Mechnaics Meeting
国/地域United States
CityTampa, FL
Period06/1/2206/1/26

ASJC Scopus subject areas

  • 航空宇宙工学
  • 宇宙惑星科学

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