DocumentCode
583566
Title
Dynamic optimization of guided missile trajectory by use of Matlab and Dynopt Toolbox
Author
Ozana, Stepan ; Pies, Martin ; Wagner, Petr
Author_Institution
Dept. of Cybern. & Biomed. Eng., VSB-Tech. Univ. of Ostrava, Ostrava, Czech Republic
fYear
2012
fDate
17-21 Oct. 2012
Firstpage
908
Lastpage
912
Abstract
The paper deals with analysis of case study concerning dynamic optimization problem using Dynopt Toolbox. Particularly it focuses on problem with free time and free end point represented by example of guided missile control in two alternatives. The paper introduces Dynopt as powerful tool for most type of dynamic optimization problem, describing the way how the problem is formulated to be ready for Dynopt syntax.
Keywords
dynamic programming; mathematics computing; missile guidance; Dynopt Toolbox; Matlab; dynamic optimization; guided missile control; guided missile trajectory; Dynamic programming; Linear programming; MATLAB; Mathematical model; Missiles; Optimization; Trajectory; Dynamic Optimization; Dynopt; Matlab;
fLanguage
English
Publisher
ieee
Conference_Titel
Control, Automation and Systems (ICCAS), 2012 12th International Conference on
Conference_Location
JeJu Island
Print_ISBN
978-1-4673-2247-8
Type
conf
Filename
6393352
Link To Document