Control of the rotation of a solid (spacecraft) with a combined optimality criterion based on quaternions

DOI10.3103/s002565442360040xOpenAlexW4387774763MaRDI QIDQ6180785

M. V. Levskii

Publication date: 22 January 2024

Published in: Mechanics of Solids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.3103/s002565442360040x

zbMATH Keywords

boundary value problemcontrol lawPontryagin maximum principlecontrol functionspacecraft reorientation

Mathematics Subject Classification ID

Matrices over special rings (quaternions, finite fields, etc.) (15B33) Control of mechanical systems (70Q05) Orbital mechanics (70M20)

Cites Work

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• Kinematically optimal spacecraft attitude control
• Modifications of the method of successive approximations for solving optimal control problems
• Time-optimal reorientation for rigid satellite with reaction wheels

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