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the related energy-optimal one is widely used in constant-specific-impulse low-thrust trajectory optimization, it is no longer applicable for variable-specific-impulse problems.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