Optimal vibration control of flexible spacecraft during a minimum-time maneuver

DOI10.1007/BF00940460zbMath0724.49023MaRDI QIDQ757823

L. Meirovitch, Y. Sharony

Publication date: 1991

Published in: Journal of Optimization Theory and Applications (Search for Journal in Brave)

zbMATH Keywords

bang-bang controlflexible spacecraftintegral feedbackperturbation approachminimum timemaneuver and vibration controltime-dependent linear quadratic regulator

Mathematics Subject Classification ID

Differential games and control (49N70) Control of mechanical systems (70Q05) Existence of optimal solutions belonging to restricted classes (Lipschitz controls, bang-bang controls, etc.) (49J30) Pursuit and evasion games (49N75)

Cites Work

• Unnamed Item
• Active control of flexible systems
• On the problem of observation spillover in self-adjoint distributed- parameter systems
• Multivariable PID estimation and control in systems with biased disturbances
• Optimal proportional plus integral control for regulator and tracking problems
• Optimal nonlinear feedback control for spacecraft attitude maneuvers
• Equations of motion for maneuvering flexible spacecraft
• Time-optimal slewing of flexible spacecraft

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