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- W2323752780 abstract "This paper presents new theoretical results which lead to a new algorithm for the computation of fuel-optimal multiple-burn orbit transfers of low and medium thrust. Theoretical results show that the traditional set of necessary conditions may be replaced with a much simpler set of equations. Intuitively, one might want to think of an optimal multiple-burn transfer problem not as one large trajectory problem, but as a sequence of optimal one-burn transfers between intermediate orbits that are optimally chosen. For spherical-body gravity, a strong relationship is shown to exist between these two problems. Based on this relationship, a new numerical method is presented which iteratively computes optimal orbit transfers. Numerical results for an 11-burn transfer are presented to demonstrate the new algorithm. (Author)" @default.
- W2323752780 created "2016-06-24" @default.
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- W2323752780 date "1996-07-29" @default.
- W2323752780 modified "2023-09-26" @default.
- W2323752780 title "Optimal non-impulsive thrust orbit transfers with large numbers of burns" @default.
- W2323752780 cites W2080612824 @default.
- W2323752780 doi "https://doi.org/10.2514/6.1996-3704" @default.
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