Dynamic optimization of guided missile trajectory by use of Matlab and Dynopt Toolbox

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 t...

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Published in:2012 12th International Conference on Control, Automation and Systems (ICCAS) pp. 908 - 912
Main Authors: Ozana, S., Pies, M., Wagner, P.
Format: Conference Proceeding
Language:English
Published: IEEE 01.10.2012
Subjects:
ISBN:9781467322478, 1467322474
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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.
AbstractList 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.
Author Ozana, S.
Pies, M.
Wagner, P.
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  givenname: P.
  surname: Wagner
  fullname: Wagner, P.
  organization: Dept. of Cybern. & Biomed. Eng., VSB-Tech. Univ. of Ostrava, Ostrava, Czech Republic
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Snippet The paper deals with analysis of case study concerning dynamic optimization problem using Dynopt Toolbox. Particularly it focuses on problem with free time and...
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StartPage 908
SubjectTerms Dynamic Optimization
Dynamic programming
Dynopt
Linear programming
Mathematical model
MATLAB
Missiles
Optimization
Trajectory
Title Dynamic optimization of guided missile trajectory by use of Matlab and Dynopt Toolbox
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