Analytical solution of the problem on an axisymmetric spacecraft attitude maneuver optimal with respect to a combined functional

DOI10.1134/S0005117921070043zbMath1475.49023OpenAlexW3193423475MaRDI QIDQ1982863

Ya. G. Sapunkov, A. V. Molodenkov

Publication date: 14 September 2021

Published in: Automation and Remote Control (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1134/s0005117921070043

zbMATH Keywords

optimal controlanalytical solutionspacecraftaxisymmetric rigid body

Mathematics Subject Classification ID

Optimality conditions for problems involving ordinary differential equations (49K15) Optimality conditions for problems involving relations other than differential equations (49K21)

Related Items (2)

Analytical quasi-optimal algorithm for the programmed control of the angular motion of a spacecraft ⋮ Control of the rotation of a solid (spacecraft) with a combined optimality criterion based on quaternions

Cites Work

• 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
• Pontryagin's maximum principle in optimal control problems of orientation of a spacecraft
• Analytical solution of the optimal slew problem for an axisymmetric spacecraft in the class of conical motions
• 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
• Unnamed Item
• Unnamed Item

This page was built for publication: Analytical solution of the problem on an axisymmetric spacecraft attitude maneuver optimal with respect to a combined functional