DocumentCode :
1795251
Title :
Applications of homotopic approach in variable-specific-impulse low-thrust trajectory optimization
Author :
Li, J.F. ; Che, Z. ; Li, H.N.
Author_Institution :
State Key Lab. of Astronaut. Dynamics, Xi´an, China
fYear :
2014
fDate :
8-10 Aug. 2014
Firstpage :
2100
Lastpage :
2104
Abstract :
Homotopic approach can greatly reduce the difficulty of solving optimal control problems. Although the technology of solving fuel-optimal problem by starting from the related energy-optimal one is widely used in constant-specific-impulse low-thrust trajectory optimization, it is no longer applicable for variable-specific-impulse problems. For the variable-specific-impulse low-thrust trajectory optimization, the homotopic variable-specific-impulse thrust model is established by proposing a cubic function of thrust as homotopic function, and then the problem can be efficiently solved by homotopic alternate algorithm. The results demonstrate that this technique can improve the probability and efficiency of finding optimal solution.
Keywords :
aerospace propulsion; electric propulsion; optimal control; space vehicles; trajectory optimisation (aerospace); constant-specific-impulse low-thrust trajectory optimization; cubic function; energy-optimal problem; fuel-optimal problem; homotopic alternate algorithm; homotopic approach; optimal control problems; spacecraft electric propulsion system; variable-specific-impulse low-thrust trajectory optimization; Earth; Equations; Mathematical model; Optimal control; Optimization; Space vehicles; Trajectory;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Guidance, Navigation and Control Conference (CGNCC), 2014 IEEE Chinese
Conference_Location :
Yantai
Print_ISBN :
978-1-4799-4700-3
Type :
conf
DOI :
10.1109/CGNCC.2014.7007501
Filename :
7007501
Link To Document :
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