Optimization of low-thrust transfers in the three body problem
Optimization of low-thrust transfers in the three body problem
- New search for: Sukhanov, A. A.
- New search for: A. Prado, A. F. B.
- New search for: Sukhanov, A. A.
- New search for: A. Prado, A. F. B.
Abstract 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.
Document information
Optimization of low-thrust transfers in the three body problem
Cosmic Research ; 46 , 5 ; 413-424
2008-09-30
12 pages
Article (Journal)
Electronic Resource
English
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