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
2000
Article (Journal)
English
BKL: | 55.60 Raumfahrttechnik / 39.00 Astronomie: Allgemeines / 50.93 Weltraumforschung | |
Local classification TIB: | 770/3520/8000 |
Optimization of Low-Thrust Interplanetary Transfers
Springer Verlag | 2000
|ENGINEERING NOTES - Low-Thrust Interplanetary Transfers, Including Escape and Capture Trajectories
Online Contents | 2007
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