Simultaneous maneuver and vibration suppression of flexible spacecraft

DOI10.1016/0307-904X(88)90051-0zbMath0661.93051OpenAlexW1975617338MaRDI QIDQ1113861

Haim Baruh, Larry M. Silverberg

Publication date: 1988

Published in: Applied Mathematical Modelling (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0307-904x(88)90051-0

zbMATH Keywords

flexible spacecraftvibration suppressionsimultaneous large-angle maneuver

Mathematics Subject Classification ID

Application models in control theory (93C95) Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10) Orbital mechanics (70M20) Control/observation systems governed by ordinary differential equations (93C15)

Cites Work

• Unnamed Item
• Active control of flexible systems
• Globally optimal control of self-adjoint distributed systems
• A comparison of control techniques for large flexible systems
• Control of Self -Adj oint Distributed-Parameter Systems
• The implementation of modal filters for control of structures
• Optimal nonlinear feedback control for spacecraft attitude maneuvers
• Uniform damping control of spacecraft
• Robust natural control of distributed systems
• Modal-Space Control of Distributed Gyroscopic Systems

This page was built for publication: Simultaneous maneuver and vibration suppression of flexible spacecraft