The explicit synthesis of stabilizing (time optimal) feedback controls for the attitude control of a rotating satellite

DOI10.1016/0096-3003(85)90030-XzbMath0575.93026OpenAlexW2006670186MaRDI QIDQ1064293

Henry Hermes, David Hogenson

Publication date: 1985

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

Full work available at URL: https://doi.org/10.1016/0096-3003(85)90030-x

zbMATH Keywords

synthesislinearizationfeedback controlrotating satellite

Mathematics Subject Classification ID

Nonlinear systems in control theory (93C10) Synthesis problems (93B50) Existence of optimal solutions belonging to restricted classes (Lipschitz controls, bang-bang controls, etc.) (49J30) Existence theories for optimal control problems involving ordinary differential equations (49J15) Orbital mechanics (70M20) Control/observation systems governed by ordinary differential equations (93C15)

Related Items (2)

Geometrical and topological methods in optimal control theory ⋮ Realizations of nonlinear systems

Cites Work

• Unnamed Item
• Unnamed Item

This page was built for publication: The explicit synthesis of stabilizing (time optimal) feedback controls for the attitude control of a rotating satellite