Optimal control of the reorientation of a spacecraft in the given time with a quadratic performance criterion related to the control and phase variables

DOI10.1134/S1064230723030097zbMath1528.93169OpenAlexW4387209650MaRDI QIDQ6178158

M. V. Levskii

Publication date: 18 January 2024

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

Full work available at URL: https://doi.org/10.1134/s1064230723030097

Mathematics Subject Classification ID

Application models in control theory (93C95) Existence theories for optimal control problems involving ordinary differential equations (49J15) Orbital mechanics (70M20) Control/observation systems governed by ordinary differential equations (93C15)

Cites Work

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• On improving the maneuverability of a space vehicle managed by inertial executive bodies
• Kinematically optimal spacecraft attitude control
• Time-optimal reorientation for rigid satellite with reaction wheels

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