Abstract A method for approximate analytical optimization of low-thrust transfers, described in [1] and based on linearization of the equations of motion, is considered. A more precise method of reducing the errors due to linearization is suggested. The method of optimization is generalized for the case of a mission to several celestial bodies.
Optimization of Low-Thrust Interplanetary Transfers
Cosmic Research ; 38 , 6 ; 584-587
2000-11-01
4 pages
Article (Journal)
Electronic Resource
English
Optimization of Low-Thrust Interplanetary Transfers
Online Contents | 2000
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