DocumentCode :
3042305
Title :
A novel algorithm for optimal design of impulsive orbit transfer using multi-phase Gauss pseudospectral method
Author :
Shen, Hongxin
Author_Institution :
Nat. Univ. of Defense Technol., Changsha, China
fYear :
2010
fDate :
8-10 June 2010
Firstpage :
588
Lastpage :
592
Abstract :
A Gauss pseudospectral method (GPM) is presented for directly solving impulsive orbit transfer problem. The Gauss pseudospectral method is applied to the multi-phase optimal control problem; the model of multi-phase control linkage conditions and more flexible solving strategy are also presented. Two typical orbit transfer problems are studied, the simulation results are compared with the available numerical prediction, and show good accuracy, rapid convergence(time consumption is several seconds), robustness with initial guess, which means that the GPM can used to generate an optimal impulsive orbit transfer trajectory through the onboard computer.
Keywords :
aerospace control; control system synthesis; optimal control; position control; Gauss pseudospectral method; impulsive orbit transfer; multiphase optimal control problem; Accuracy; Couplings; Optimization; Orbits; Robustness; Space vehicles; Trajectory;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Systems and Control in Aeronautics and Astronautics (ISSCAA), 2010 3rd International Symposium on
Conference_Location :
Harbin
Print_ISBN :
978-1-4244-6043-4
Electronic_ISBN :
978-1-4244-7505-6
Type :
conf
DOI :
10.1109/ISSCAA.2010.5633101
Filename :
5633101
Link To Document :
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