Adaptive control for autonomous rendezvous of spacecraft on elliptical orbit

DOI10.1007/S10409-009-0235-9zbMath1178.70090OpenAlexW2395790728MaRDI QIDQ1049642

Shan Lu, Shi-Jie Xu

Publication date: 13 January 2010

Published in: Acta Mechanica Sinica (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s10409-009-0235-9

zbMATH Keywords

adaptive controlelliptical orbitautonomous rendezvousLyapunov approachgain factor

Mathematics Subject Classification ID

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

Related Items (1)

Multi-objective output feedback control for autonomous spacecraft rendezvous

Cites Work

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• Study on relative orbital configuration in satellite formation flying
• Adaptive output feedback control of nonlinear systems represented by input-output models
• Adaptive output tracking of inherently nonlinear systems with nonlinear parameterization
• Optimal four-impulse fixed-time rendezvous in the vicinity of a circular orbit.
• Optimal two- and three-impulse fixed-time rendezvous in the vicinityof a circular orbit

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