Analytical quasi-optimal solution of the problem of the time-optimal rotation of a spacecraft

DOI10.1134/S1064230721030114zbMath1493.70087OpenAlexW3194442727MaRDI QIDQ2239226

A. V. Molodenkov, Ya. G. Sapunkov

Publication date: 3 November 2021

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

Full work available at URL: https://doi.org/10.1134/s1064230721030114

Mathematics Subject Classification ID

Variable mass, rockets (70P05)

Related Items (1)

Analytical quasi-optimal algorithm for the programmed control of the angular motion of a spacecraft

Cites Work

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• Analytical solution of the of optimal slew problem of a spherically symmetric spacecraft in the class of conical motions
• Analytical approximate solution of the problem of a spacecraft's optimal turn with arbitrary boundary conditions
• Synthesis of the optimal control of the spacecraft orientation using combined criteria of quality
• Analytic solution of a problem on the time-optimal slewing of an axisymmetric spacecraft in the class of conical motions
• Analytical solution of the time-optimal slew problem of a spherically symmetric spacecraft in the class of conical motions
• Restricted quadratic optimal control of a spacecraft turning in a fixed time period
• A shooting method for solving two-point boundary-value problems arising from non-singular bang-bang optimal control problems

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