Optimization of low-thrust transfers in the three body problem

Details Optimization of low-thrust transfers in the three body problem Optimization of low-thrust transfers in the three body problem

Oct 2008

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2008cosre..46..413s&link_type=abstract

Cosmic Research, Volume 46, Issue 5, pp.413-424

Computer Science

Numerical Analysis

45.40. Gj

Scientific paper

We consider transfers with low thrust in an arbitrary field of forces. The modified method of transporting trajectory [1 4] is used for optimization of the transfers. The complexity of finding the transporting trajectory of a preset type can be the main obstacle to application of this method. This challenge is solved for the three-body problem in the Hill motion model. Numerical analysis of the method is performed using an example of the transfers to halo-orbits around the solar-terrestrial libration points.

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