Radially accelerated optimal feedback orbits in central gravity field with linear drag

DOI10.1007/S10569-008-9161-6zbMath1160.70011OpenAlexW2066604757MaRDI QIDQ1011851

Francesco Topputo, Ashraf Owis, Franco Bernelli-Zazzera

Publication date: 14 April 2009

Published in: Celestial Mechanics and Dynamical Astronomy (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s10569-008-9161-6

zbMATH Keywords

linearizationquadratic objective functiongenerating function methodanalytic closed-loop solutions

Mathematics Subject Classification ID

Feedback control (93B52) Control of mechanical systems (70Q05) Orbital mechanics (70M20)

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Cites Work

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• Fuel-optimal rendezvous near a point in general Keplerian orbit
• An analytic solution to the classical two-body problem with drag
• Feedback control methodologies for nonlinear systems

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