DocumentCode
554233
Title
Improved parameterization method and its application on solving optimal control problem
Author
Hu Chao-jiang ; Yang Quan-fa ; Li Xiao-chong ; Yuan You-zhi
Author_Institution
Beijing Aeronaut. Technol. Res. Center, Beijing, China
Volume
1
fYear
2011
fDate
12-14 Aug. 2011
Firstpage
437
Lastpage
439
Abstract
The mathematics fundamentals of solving optimal control(OC) problem by parameterization method is easy to be understood, but a nonlinear programming(NLP) problem is usually hard to be solved because the dimension derived from parameterization method are too high. The characteristics of improved method is that only parameterizes the control variables. The dimensions of a NLP problem will be reduced greatly if the improved parameterization method is employed, then the problem will become easy to solve. The improved method has been successfully applied to solve a problem of an aircraft optimal landing trajectory in penetrating wind shear.
Keywords
aircraft landing guidance; nonlinear programming; optimal control; aircraft optimal landing trajectory; nonlinear programming problem; optimal control problem; parameterization method; wind shear penetration; Aerospace control; Aircraft; Differential equations; Force; Heuristic algorithms; Optimal control; Process control; improved parameterization method; optimal control; wind shear;
fLanguage
English
Publisher
ieee
Conference_Titel
Electronic and Mechanical Engineering and Information Technology (EMEIT), 2011 International Conference on
Conference_Location
Harbin, Heilongjiang, China
Print_ISBN
978-1-61284-087-1
Type
conf
DOI
10.1109/EMEIT.2011.6022912
Filename
6022912
Link To Document