Kinematically optimal spacecraft attitude control

DOI10.1134/S1064230714050116zbMath1317.49028MaRDI QIDQ2515397

M. V. Levskii

Publication date: 5 August 2015

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

Mathematics Subject Classification ID

Variable mass, rockets (70P05) Optimality conditions for problems involving ordinary differential equations (49K15)

Related Items (4)

Optimal control of the reorientation of a spacecraft in the given time with a quadratic performance criterion related to the control and phase variables ⋮ Control of the rotation of a solid (spacecraft) with a combined optimality criterion based on quaternions ⋮ Optimal control of the angular momentum for a solid (spacecraft) performing a spatial turn ⋮ Statistical analysis of diffusion systems with invariants

Cites Work

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• On optimal spacecraft damping
• 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

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