Analytical solution for power-limited optimal rendezvous near an elliptic orbit

DOI10.1007/S10957-008-9369-3zbMath1191.49043OpenAlexW1998238579MaRDI QIDQ937135

B. E. Eshmatov

Publication date: 20 August 2008

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

Full work available at URL: https://doi.org/10.1007/s10957-008-9369-3

zbMATH Keywords

eccentric orbitsLambert \(W\) functionTschauner-Hempel equationsoptimal rendezvouspower-limited propulsion

Mathematics Subject Classification ID

Optimal feedback synthesis (49N35) Variable mass, rockets (70P05) Existence theories for optimal control problems involving ordinary differential equations (49J15)

Related Items (3)

Cluster flight control for fractionated spacecraft on an elliptic orbit ⋮ Low-thrust transfers to southern \(L_2\) near-rectilinear halo orbits facilitated by invariant manifolds ⋮ An optimal control approach to spacecraft rendezvous on elliptical orbit

Cites Work

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• A closed-form solution for minimum-fuel, constant-thrust trajectories
• Some optimal low-acceleration rendezvous maneuvers

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