Arbitrary fuel-optimal attitude maneuvering of a non-symmetric space vehicle in a vehicle-fixed coordinate frame

DOI10.1016/S0005-1098(02)00247-9zbMath1019.93034MaRDI QIDQ1868067

Ioslovich, Ilya

Publication date: 27 April 2003

Published in: Automatica (Search for Journal in Brave)

zbMATH Keywords

optimal controlattitude controlrigid body rotationKrotov-Bellman functioncyclic sliding modespassive integral methodspace vehicle maneuvering

Mathematics Subject Classification ID

Application models in control theory (93C95) Variable structure systems (93B12)

Related Items (1)

Long time missions and the fuel-optimal attitude maneuvering in a swinging mode

Cites Work

• Optimal stabilization of rigid body attitude
• Minimum fuel spacecraft reorientation
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