The problem of optimal control of the orientation of an orbit of a spacecraft as a deformable figure

DOI10.1134/S106423070804014XzbMath1178.49022MaRDI QIDQ734022

Yu. N. Chelnokov, Yu. V. Afanas'eva

Publication date: 19 October 2009

Published in: Journal of Computer and Systems Sciences International (Search for Journal in Brave)

zbMATH Keywords

Pontryagin's maximum principleoptimal control of the orbit orientation

Mathematics Subject Classification ID

Applications of optimal control and differential games (49N90) Variable mass, rockets (70P05) Optimality conditions for problems involving ordinary differential equations (49K15)

Related Items (1)

Quaternion methods and regular models of celestial mechanics and space flight mechanics: the use of Euler (Rodrigues-Hamilton) parameters to describe orbital (trajectory) motion. I: Review and analysis of methods and models and their applications

Cites Work

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