Stability of the control of a plane turn of a spacecraft

DOI10.1016/0021-8928(91)90073-4zbMath0850.70289OpenAlexW1970557851MaRDI QIDQ1190085

K. B. Alekseev, S. A. Agafonov, N. V. Nikolaev

Publication date: 26 September 1992

Published in: Journal of Applied Mathematics and Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0021-8928(91)90073-4

Mathematics Subject Classification ID

Control of mechanical systems (70Q05) Orbital mechanics (70M20)

Related Items (2)

Optimal control of a rigid spacecraft programmed motion without angular velocity measurements ⋮ Optimal control of a programmed motion of a rigid spacecraft using redundant kinematics parameterizations

Cites Work

• Some three-dimensional inclusion problems in elasticity
• Asymptotic behavior of solutions of elliptic equations of the second order close to a boundary. I
• Stress-strain state near the tip of a perfectly rigid three-dimensional spike introduced into an elastic body
• Unnamed Item
• Unnamed Item
• Unnamed Item
• Unnamed Item
• Unnamed Item
• Unnamed Item
• Unnamed Item

This page was built for publication: Stability of the control of a plane turn of a spacecraft