Derivation of the Optimal Guidance Law for Space Vehicle Based on a DAE
碩士 === 國立臺灣海洋大學 === 電機工程學系 === 93 === The purpose of this thesis The purpose of this thesis is two-fold: to analyze the numerical method for nonlinear differential algebraic equations (DAE's) and to solve the optimal control problem in a DAE framework. In particular, the optimal guidance law fo...
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ndltd-TW-093NTOU54420412016-06-01T04:25:06Z http://ndltd.ncl.edu.tw/handle/81344031623539762221 Derivation of the Optimal Guidance Law for Space Vehicle Based on a DAE 飛行載具之最佳化控制法則-使用微分代數方程式 Wei-Lun Jhu 朱偉綸 碩士 國立臺灣海洋大學 電機工程學系 93 The purpose of this thesis The purpose of this thesis is two-fold: to analyze the numerical method for nonlinear differential algebraic equations (DAE's) and to solve the optimal control problem in a DAE framework. In particular, the optimal guidance law for air-craft dynamics is derived based on a DAE approach. We will reformulate the problem as a Hamiltonian DAE system. After establishing the system of aircraft dynamics, we can derive the optimal guidance law of the system by numerical method. The numerical method is mainly based on the backward differential formulas (BDF). Chee-Fai Yung He-Sheng Wang 容志輝 王和盛 2005 學位論文 ; thesis 90 en_US |
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碩士 === 國立臺灣海洋大學 === 電機工程學系 === 93 === The purpose of this thesis The purpose of this thesis is
two-fold: to analyze the numerical method for nonlinear
differential algebraic equations (DAE's) and to solve the optimal
control problem in a DAE framework. In particular, the optimal
guidance law for air-craft dynamics is derived based on a DAE
approach. We will reformulate the problem as a Hamiltonian DAE
system. After establishing the system of aircraft dynamics, we can
derive the optimal guidance law of the system by numerical
method. The numerical method is mainly based on the backward
differential formulas (BDF).
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author2 |
Chee-Fai Yung |
author_facet |
Chee-Fai Yung Wei-Lun Jhu 朱偉綸 |
author |
Wei-Lun Jhu 朱偉綸 |
spellingShingle |
Wei-Lun Jhu 朱偉綸 Derivation of the Optimal Guidance Law for Space Vehicle Based on a DAE |
author_sort |
Wei-Lun Jhu |
title |
Derivation of the Optimal Guidance Law for Space Vehicle Based on a DAE |
title_short |
Derivation of the Optimal Guidance Law for Space Vehicle Based on a DAE |
title_full |
Derivation of the Optimal Guidance Law for Space Vehicle Based on a DAE |
title_fullStr |
Derivation of the Optimal Guidance Law for Space Vehicle Based on a DAE |
title_full_unstemmed |
Derivation of the Optimal Guidance Law for Space Vehicle Based on a DAE |
title_sort |
derivation of the optimal guidance law for space vehicle based on a dae |
publishDate |
2005 |
url |
http://ndltd.ncl.edu.tw/handle/81344031623539762221 |
work_keys_str_mv |
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