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Optimal Low-Thrust Limited-Power Transfers between Arbitrary Elliptic Coplanar OrbitsIn this work, a complete first order analytical solution, which includes the short periodic terms, for the problem of optimal low-thrust limited-power transfers between arbitrary elliptic coplanar orbits in a Newtonian central gravity field is obtained through Hamilton-Jacobi theory and a perturbation method based on Lie series.
Document ID
20080012661
Document Type
Conference Paper
Authors
daSilvaFernandes, Sandro (Instituto Tecnologico de Aeronautica Sao Jose dos Campos, Brazil)
dasChagasCarvalho, Francisco (Instituto Tecnologico de Aeronautica Sao Jose dos Campos, Brazil)
Date Acquired
August 24, 2013
Publication Date
September 24, 2007
Publication Information
Publication: Proceedings of the 20th International Symposium on Space Flight Dynamics
Subject Category
Astrodynamics
Distribution Limits
Public
Copyright
Public Use Permitted.

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IDRelationTitle20080012629Analytic PrimaryProceedings of the 20th International Symposium on Space Flight Dynamics