Low thrust mission analysis using an analytical trajectory optimization model

1970 ◽  
Author(s):  
G. HAZELRIGG, JR. ◽  
A. KORNHAUSER ◽  
P. LION
2013 ◽  
Vol 756-759 ◽  
pp. 3466-3470
Author(s):  
Xu Min Song ◽  
Qi Lin

The trajcetory plan problem of spece reandezvous mission was studied in this paper using nolinear optimization method. The optimization model was built based on the Hills equations. And by analysis property of the design variables, a transform was put forward , which eliminated the equation and nonlinear constraints as well as decreaseing the problem dimensions. The optimization problem was solved using Adaptive Simulated Annealing (ASA) method, and the rendezvous trajectory was designed.The method was validated by simulation results.


2006 ◽  
Vol 43 (1) ◽  
pp. 121-129 ◽  
Author(s):  
Byoungsam Woo ◽  
Victoria L. Coverstone ◽  
Michael Cupples

2020 ◽  
Vol 21 (3) ◽  
pp. 142-152
Author(s):  
Nicholas J. Potter ◽  
Guanghua Yan ◽  
Hongcheng Liu ◽  
Haitham Alahmad ◽  
Darren L. Kahler ◽  
...  

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