DocumentCode
536235
Title
Multi-pulse maneuver orbit optimization based on a new hybrid algorithm
Author
Chunke, Li
Author_Institution
Coll. of Astronaut., Northwestern Polytech. Univ., Xi´´an, China
Volume
1
fYear
2010
fDate
29-31 Oct. 2010
Firstpage
577
Lastpage
580
Abstract
For the Lambert method based on two-body supposition and do not account for actual orbit perturbation affection, we put forward a new orbit maneuver optimization method which suits for an arbitrary number impulse maneuver accounting for perturbation affection. Firstly, we describe the maneuver process by equation accounting for perturbation affection. Then we combine the equation with nonlinear programming with constraints and get a set of optimal equations. Thirdly, we use a new hybrid algorithm to solve the optimal problem, which combine SQP with PSO and can reinforces the search accuracy and improves the convergence. Finally, the simulation results show that this method is feasible and can be used to solve multi-impulse perturbation orbit transform problem efficiently.
Keywords
artificial satellites; nonlinear programming; perturbation techniques; search problems; tracking; Lambert method; PSO; SQP; multiimpulse perturbation orbit transform; multipulse maneuver orbit optimization; nonlinear programming; orbit perturbation affection; Multi-pulse orbit maneuver; Nonlinear programming with constraints; perturbation affection;
fLanguage
English
Publisher
ieee
Conference_Titel
Intelligent Computing and Intelligent Systems (ICIS), 2010 IEEE International Conference on
Conference_Location
Xiamen
Print_ISBN
978-1-4244-6582-8
Type
conf
DOI
10.1109/ICICISYS.2010.5658447
Filename
5658447
Link To Document