Analytic solution for fuel-optimal reconfiguration in relative motion

DOI10.1007/s10957-008-9482-3zbMath1178.93011OpenAlexW2010672295MaRDI QIDQ1035873

J. Blot

Publication date: 4 November 2009

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

Full work available at URL: http://orbi.ulg.ac.be/handle/2268/193393

zbMATH Keywords

fundamental matrixsatellite formation flyingcontinuous low-level thrustfuel-optimal reconfigurationslinearized relative equations of motion

Mathematics Subject Classification ID

Applications of optimal control and differential games (49N90) Decentralized systems (93A14)

Related Items (2)

Spacecraft formation flying reconfiguration with extended and impulsive maneuvers ⋮ An optimal control approach to spacecraft rendezvous on elliptical orbit

Cites Work

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• State Transition Matrices for Terminal Rendezvous Studies: Brief Survey and New Example
• Fuel optimal manoeuvres for multiple spacecraft formation reconfiguration using multi‐agent optimization
• Stability of a spinning body containing elastic parts via Liapunov'sdirect method

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