In this paper we develop the coupled orbital/attitude dynamics of a multi-body solar sail spacecraft (sailcraft) under the gravitational attraction of a single central body.
Solar sail dynamics and control using a boom mounted bus articulated by a bi-state two-axis gimbal and reaction wheel
2002 AIAA/AAS Astrodynamics Conference
2002-08-05
Conference paper
No indication
English
British Library Conference Proceedings | 2002
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