Optimal orientation control of a space vehicle with restrictions on the control and phase variables

DOI10.1134/S1064230721030096zbMath1487.49058OpenAlexW4200609779MaRDI QIDQ2134326

M. V. Levskii

Publication date: 3 May 2022

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

Full work available at URL: https://doi.org/10.1134/s1064230721030096

zbMATH Keywords

spacecraftreorientation

Mathematics Subject Classification ID

Variational principles of physics (49S05) Optimality conditions for problems involving relations other than differential equations (49K21)

Cites Work

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• Terminal synthesis of orbital orientation for a spacecraft
• Analytic solution of a problem on the time-optimal slewing of an axisymmetric spacecraft in the class of conical motions
• A solution of the optimal turn problem of an axially symmetric spacecraft with bounded and pulse control under arbitrary boundary conditions
• Optimal Large-Angle Single-Axis Rotational Maneuvers of Flexible Spacecraft
• Gradient projection-based performance improvement for JLQ problems

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