DocumentCode
550663
Title
Rapid gliding trajectory optimization via hp-adaptive pseudospectral method
Author
Hong Bei ; Xin Wan-Qing
Author_Institution
China Acad. of Launch Vehicle Technol., Beijing, China
fYear
2011
fDate
22-24 July 2011
Firstpage
1956
Lastpage
1961
Abstract
Based on hp-adaptive pseudospectral method, this paper presents a new optimal control method to solve the rapid gliding trajectory optimization. In order to meet the speed and precision requirements, this new theory combines the global pseudospectral method with the finite element method, adopts double layer optimization strategy to adjust adaptively the segment breaks and the polynomial degree in each segment. The simulation based on hp-adaptive pseudospectral method is carried out, the result is validated by Pontryagin minimum principle, and compared with the result of Gauss pseudospectral method. The results show that the algorithm is robust, has fast convergence and not sensitive to the initial control values. The method in this paper has a great value in the practical applications.
Keywords
Gaussian processes; adaptive systems; finite element analysis; maximum principle; optimisation; position control; Gauss pseudospectral method; Pontryagin minimum principle; double layer optimization strategy; finite element method; global pseudospectral method; hp-adaptive pseudospectral method; optimal control method; precision requirements; rapid gliding trajectory optimization; Convergence; Electronic mail; Finite element methods; Optimal control; Optimization; Robustness; Trajectory; Gliding Trajectory; Optimal Control; Rapid Optimization; hp-Adaptive Pseudospectral Method;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference (CCC), 2011 30th Chinese
Conference_Location
Yantai
ISSN
1934-1768
Print_ISBN
978-1-4577-0677-6
Electronic_ISBN
1934-1768
Type
conf
Filename
6001002
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