Referenced Items are not available for this document.
The paper adopts the energy shaping method to rotational motion control of a spacecraft. The configuration manifold considered in this paper is the 3-sphere. The quaternion and its conjugate momentum are used for global representation of motion in the canonical form. The design algorithm presented is validated for three typical attitude control objectives: stabilization in an inertial coordinate system, slew maneuver with obstacle avoidance, and active vibration damping for a low Earth orbit spacecraft
Published in:
Decision and Control, 2001. Proceedings of the 40th IEEE Conference on
(Volume:5
)
Date of Conference: 2001
- Page(s):
- 4610 - 4615 vol.5
- Meeting Date :
- 04 Dec 2001-07 Dec 2001
- Print ISBN:
- 0-7803-7061-9
- INSPEC Accession Number:
- 7204985
- Conference Location :
- Orlando, FL
- Digital Object Identifier :
- 10.1109/.2001.980931
- Product Type:
- Conference Publications
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