Time-Optimal De-tumbling Control of a Rigid Spacecraft

DOI10.1177/1077546307080034zbMath1229.70089OpenAlexW2126032250MaRDI QIDQ3110969

Chia-Ju Wu, Chi-Ching Yang

Publication date: 17 January 2012

Published in: Journal of Vibration and Control (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1177/1077546307080034

zbMATH Keywords

nonlinear programmingrigid spacecrafttime-optimalde-tumbling control

Mathematics Subject Classification ID

Free motion of a rigid body (70E15) Control of mechanical systems (70Q05)

Cites Work

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• A computationally efficient numerical algorithm for the minimum-time control problem of continuous systems
• Optimal stabilization of rigid body attitude
• Optimal nonlinear feedback control for spacecraft attitude maneuvers
• Robust attitude stabilization of spacecraft using nonlinear quaternion feedback
• Attitude Control of a Spacecraft with Two Reaction Wheels

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