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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Vydané v:	IEEE transactions on aerospace and electronic systems Ročník 46; číslo 3; s. 1097 - 1109
Hlavní autori:	Yoonsoo Kim, Mesbahi, M, Singh, G, Hadaegh, F Y
Médium:	Journal Article
Jazyk:	English
Vydavateľské údaje:	New York IEEE 01.07.2010 The Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Predmet:	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
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