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
Aufsatz (Zeitschrift)
Englisch
BKL: | 50.93 Weltraumforschung / 39.00 Astronomie: Allgemeines / 55.60 Raumfahrttechnik | |
Lokalklassifikation TIB: | 770/3520/8000 |
Optimization of Low-Thrust Interplanetary Transfers
Springer Verlag | 2000
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