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
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;
Conference_Titel :
Control Conference (CCC), 2011 30th Chinese
Conference_Location :
Yantai
Print_ISBN :
978-1-4577-0677-6
Electronic_ISBN :
1934-1768