DocumentCode :
724442
Title :
Trajectories optimization of hypersonic vehicle based on a hybrid optimization algorithm of PSO and SQP
Author :
Linshuang Feng ; Lei Liu ; Yongji Wang
Author_Institution :
Nat. Key Lab. of Sci. & Technol. on Multispectral Inf. Process., Huazhong Univ. of Sci. & Technol., Wuhan, China
fYear :
2015
fDate :
23-25 May 2015
Firstpage :
4518
Lastpage :
4522
Abstract :
We discuss the trajectory optimization problems in the climb segment of the hypersonic vehicle in this paper. First of all, we analyze the hypersonic vehicle model. The strength of the PSO algorithm (Particle Swarm Optimization, PSO) is its strong global optimization ability, but its local optimization ability is relatively weak. The SQP algorithm (Sequential Quadratic Programming, SQP) is quite the opposite, and it has high requirements of the initial trajectory. So we propose a hybrid optimization algorithm of PSO and SQP which combine the advantages of PSO and SQP, while improving the quality of the optimal trajectory.
Keywords :
aircraft control; optimal control; particle swarm optimisation; quadratic programming; trajectory optimisation (aerospace); PSO algorithm; SQP algorithm; climb segment; global optimization; hybrid optimization algorithm; hypersonic vehicle model; local optimization; optimal trajectory; particle swarm optimization; sequential quadratic programming; trajectory optimization problem; Electronic mail; Particle swarm optimization; Quadratic programming; Vehicles; Hybrid optimization; Hypersonic aircraft; PSO; SQP; Trajectory optimization;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control and Decision Conference (CCDC), 2015 27th Chinese
Conference_Location :
Qingdao
Print_ISBN :
978-1-4799-7016-2
Type :
conf
DOI :
10.1109/CCDC.2015.7162721
Filename :
7162721
Link To Document :
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