DocumentCode :
2325469
Title :
Constrained global optimization of low-thrust interplanetary trajectories
Author :
Yam, Chit Hong ; Di Lorenzo, David ; Izzo, Dario
Author_Institution :
Adv. Concepts Team of the Eur. Space Agency, ESTEC, Noordwijk, Netherlands
fYear :
2010
fDate :
18-23 July 2010
Firstpage :
1
Lastpage :
7
Abstract :
The optimization of spacecraft trajectories can be formulated as a global optimization task. The complexity of the problem depends greatly on the problem formulation, on the spacecraft route to its final target planet, and on the type of engine and power system that is available on-board the spacecraft. Few attempts have been made to use a global optimization framework to design trajectories that make use of electric propulsion to propel the spacecraft between planets because of the large scale and extreme complexity of the resulting nonlinear programming problem. The presence of a high number of nonlinear constraints, in particular, requires a special attention with respect to the global optimization technique adopted. Here we use the Sims-Flanagan transcription method to produce the nonlinear programming problem and we make use of two global optimization algorithms, basin hopping and simulated annealing with adaptive neighborhood to attempt exploring efficiently the solution space. Both algorithms are hybridized with a local search. We consider two different interplanetary trajectories, an Earth-Earth-Jupiter transfer and an Earth-Earth-Earth-Jupiter transfer with a nuclear electric propulsion spacecraft inspired by the Jupiter Icy Moons Orbiter. For both problems, our approach is able to explore automatically the vast solution space producing a large number of trajectories in a large range of final mass and flight times.
Keywords :
nonlinear programming; position control; simulated annealing; space vehicles; Earth-Earth-Earth-Jupiter transfer; Jupiter Icy Moons Orbiter; Sims-Flanagan transcription method; basin hopping; constrained global optimization; low-thrust interplanetary trajectories; nonlinear programming; nuclear electric propulsion spacecraft; simulated annealing; spacecraft route; spacecraft trajectories; Earth; Jupiter; Leg; Optimization; Propulsion; Space vehicles; Trajectory;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Evolutionary Computation (CEC), 2010 IEEE Congress on
Conference_Location :
Barcelona
Print_ISBN :
978-1-4244-6909-3
Type :
conf
DOI :
10.1109/CEC.2010.5586019
Filename :
5586019
Link To Document :
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