On the Convex Parameterization of Constrained Spacecraft Reorientation

Guiding the rotational motion of a spacecraft subject to constraints on its permissible orientation often leads to nonconvex optimal control problems. In this paper, we consider convex parameterizations of sets associated with the constrained rigid body orientations. We then elaborate on ramificatio...

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Bibliographic Details
Published in:	IEEE transactions on aerospace and electronic systems Vol. 46; no. 3; pp. 1097 - 1109
Main Authors:	Yoonsoo Kim, Mesbahi, M, Singh, G, Hadaegh, F Y
Format:	Journal Article
Language:	English
Published:	New York IEEE 01.07.2010 The Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subjects:	Africa Algorithms Constraints Infrared heating Instruments Laws Orientation Parametrization Propulsion Rigid-body dynamics Space cooling Space heating Space missions Space technology Space vehicles Spacecraft Star trackers Telescopes
ISSN:	0018-9251, 1557-9603
Online Access:	Get full text
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