On the problem of optimal spacecraft attitude control

DOI10.1134/S1064230716010093zbMath1387.49057MaRDI QIDQ1743047

M. V. Levskii

Publication date: 12 April 2018

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

zbMATH Keywords

spacecraft reorientationoptimal spacecraft slew maneuver

Mathematics Subject Classification ID

Applications of optimal control and differential games (49N90) Variable mass, rockets (70P05) Control problems involving ordinary differential equations (34H05)

Related Items

The optimal in terms of fuel consumption approach to reorientation of a spacecraft based on the nonlinear boundary value problem solution

Cites Work

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• Pontryagin's maximum principle in optimal control problems of orientation of a spacecraft
• Synthesis of spacecraft reorientation algorithms using the concept of the inverse dynamic problem