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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Abstract	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 ramifications of such a parameterization in the development of steering laws for autonomous spacecraft reorientation that are based on convex optimization algorithms. Such problems appear in almost every space science mission equipped with heat- or light-sensitive instruments, e.g., cryogenically cooled infrared telescopes, star trackers, and low-energy ion composition analyzers. An example, demonstrating the viability of the proposed algorithm for constrained multiple spacecraft reorientations concludes the work presented here.
AbstractList	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 ramifications of such a parameterization in the development of steering laws for autonomous spacecraft reorientation that are based on convex optimization algorithms. Such problems appear in almost every space science mission equipped with heat- or light-sensitive instruments, e.g., cryogenically cooled infrared telescopes, star trackers, and low-energy ion composition analyzers. An example, demonstrating the viability of the proposed algorithm for constrained multiple spacecraft reorientations concludes the work presented here.
Author	Singh, G Hadaegh, F Y Mesbahi, M Yoonsoo Kim
Author_xml	– sequence: 1 surname: Yoonsoo Kim fullname: Yoonsoo Kim organization: Dept. of Mech. & Mechatron. Eng., Univ. of Stellenbosch, Stellenbosch, South Africa – sequence: 2 givenname: M surname: Mesbahi fullname: Mesbahi, M email: mesbahi@aa.washington.edu organization: Dept. of Aeronaut. & Astronaut., Univ. of Washington, Seattle, WA, USA – sequence: 3 givenname: G surname: Singh fullname: Singh, G organization: Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA – sequence: 4 givenname: F Y surname: Hadaegh fullname: Hadaegh, F Y organization: Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
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Cites_doi	10.1109/9.83532 10.1137/1.9781611970777 10.1515/9780691211701 10.2514/3.20073 10.1016/j.conengprac.2003.12.006 10.2514/2.5059 10.2514/3.19868 10.1109/TAC.2004.825959 10.1109/TAES.1973.309659 10.1016/S0094-5765(00)00087-4 10.2514/3.55974 10.1007/BF02592331 10.2514/6.1997-3526 10.1016/S0011-2275(99)00012-0 10.1109/9.90228 10.2514/3.21283 10.1109/7.259519 10.2514/2.4469 10.1016/S0005-1098(97)00157-X
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References	ref13 sorensen (ref21) 1993 ref12 ref14 ref11 ref10 frakes (ref7) 1992 ref2 ref17 ref18 frazzoli (ref8) 2001 ahmed (ref1) 1998 cheng (ref5) 2004 ref24 ref23 ref26 kuipers (ref15) 1999 ref25 ref20 spindler (ref22) 1998; 100 (ref19) 0 ref9 ref4 ref3 ref6 mayne (ref16) 1997; 33
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SubjectTerms	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
Title	On the Convex Parameterization of Constrained Spacecraft Reorientation
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