Optimization of the transfer trajectory of a low-thrust spacecraft for research of Jupiter using an Earth gravity-assist maneuver

2014 ◽  
Vol 48 (7) ◽  
pp. 606-612 ◽  
Author(s):  
M. S. Konstantinov ◽  
A. A. Orlov
Author(s):  
Guilherme Marcos Neves ◽  
Denilson Paulo Souza dos Santos

In this paper, it was studied the optimization of the cost of interplanetary missions with emphasis on reducing fuel consumption. To achieve this goal, a genetic algorithm was implemented to optimize the total impulse of orbital transfer. It was implemented a case of sending a space vehicle from Earth to a another planet using a gravity assist maneuver (swing by), in this paper it was chose sending a spacecraft from Earth to Mars with a close approach to the Venus. The method employed can be used for impulsive interplanetary missions in general, and so the solution found can become an initial solution for numerical methods of optimization of low thrust maneuvers


2006 ◽  
Vol 43 (1) ◽  
pp. 121-129 ◽  
Author(s):  
Byoungsam Woo ◽  
Victoria L. Coverstone ◽  
Michael Cupples

2009 ◽  
Vol 32 (2) ◽  
pp. 616-625 ◽  
Author(s):  
Ian Carnelli ◽  
Bernd Dachwald ◽  
Massimiliano Vasile

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