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 :
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