DocumentCode :
2849389
Title :
Time-Optimal Multi-impulse Rendezvous Based on Genetic Algorithm
Author :
Bao-jun, Li ; Peng, Shi ; Hao, Zhang ; Yu-shan, Zhao
Author_Institution :
Sch. of Astronaut., Beihang Univ., Beijing, China
Volume :
2
fYear :
2010
fDate :
13-14 Oct. 2010
Firstpage :
777
Lastpage :
781
Abstract :
For the short-range rendezvous problem, an approach of time-optimal multi-impulse rendezvous was put forward using hybrid genetic algorithm. Firstly, based on the state transition matrix of T-H equation, the mathematical models of time-optimal multi-impulse rendezvous was established and transformed into a nonlinear optimization problem, In order to obtain the global solution efficiently, a hybrid optimizer combining the advantages of genetic algorithm and sequential quadratic programming algorithm is employed. The hybrid genetic algorithm was brought in for the global optimization of this problem to solve the impulse vectors and time needed for the rendezvous, finally, through the example of numerical simulation, the accuracy of the model of multi-impulse rendezvous and the validity of hybrid genetic algorithm to solve the problem were verified.
Keywords :
aerospace control; artificial satellites; genetic algorithms; matrix algebra; quadratic programming; time optimal control; transient response; T-H equation; hybrid genetic algorithm; impulse vector; nonlinear optimization problem; sequential quadratic programming algorithm; short range rendezvous problem; state transition matrix; time optimal multi-impulse rendezvous; Equations; Fuels; Genetic algorithms; Mathematical model; Optimization; Orbits; Satellites; genetic algorithm; global optimization; multi-impulse rendezvous; time-optimal;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Intelligent System Design and Engineering Application (ISDEA), 2010 International Conference on
Conference_Location :
Changsha
Print_ISBN :
978-1-4244-8333-4
Type :
conf
DOI :
10.1109/ISDEA.2010.222
Filename :
5743525
Link To Document :
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