DocumentCode :
3369294
Title :
Applying hybrid genetic algorithm to constrained trajectory optimization
Author :
Jianke Sha ; Min Xu
Author_Institution :
Coll. of Astronaut., Northwestern Polytech. Univ., Xi´an, China
Volume :
7
fYear :
2011
fDate :
12-14 Aug. 2011
Firstpage :
3792
Lastpage :
3795
Abstract :
Trajectory optimization is a typical optimal control problem. Aiming at the slow convergence characteristics and the poor local searching ability of a basic genetic algorithm, this paper proposed a new hybrid global-local optimization algorithm by coming genetic algorithm and complex algorithm to improve the convergence rate of genetic algorithm. The hybrid way adopted serial hybrid pattern in this paper. It can mean that the optimal solution of genetic algorithm is submitted as an initial parameter set to complex algorithm for refinement. In order to validate algorithm, hybrid genetic algorithm applied to lunar soft landing trajectory optimization problem. Simulation results demonstrate that the methodology and algorithms take on fast convergence rate and high optimization precision.
Keywords :
genetic algorithms; optimal control; position control; adopted serial hybrid pattern; complex algorithm; constrained trajectory optimization precision; convergence characteristics; convergence rate; hybrid genetic algorithm; hybrid global-local optimization algorithm; local searching ability; lunar soft landing trajectory optimization problem; optimal control problem; optimal solution; Algorithm design and analysis; Convergence; Genetic algorithms; Moon; Optimal control; Optimization; Trajectory; complex algorithm; genetic algorithm; trajectory optimization;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Electronic and Mechanical Engineering and Information Technology (EMEIT), 2011 International Conference on
Conference_Location :
Harbin, Heilongjiang
Print_ISBN :
978-1-61284-087-1
Type :
conf
DOI :
10.1109/EMEIT.2011.6023884
Filename :
6023884
Link To Document :
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