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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Main Authors: Wei-Lun Jhu, 朱偉綸
Other Authors: Chee-Fai Yung
Format: Others
Language:en_US
Published: 2005
Online Access:http://ndltd.ncl.edu.tw/handle/81344031623539762221
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spelling 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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description 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).
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
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