運用奇異線性指數二次高斯及迴路轉移函數回歸法從事傾斜轉彎自動駕儀之設計研究

碩士 === 國防大學中正理工學院 === 電子工程研究所 === 91 === In this thesis, a bank-to-turn missile autopilot is designed by using the Generalized Singular Linear Exponential Quadratic Gaussian and Loop Transfer Recovery techniques. The Generalized Singular Linear Exponential Quadratic Gaussian method is adopted for tw...

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Main Authors: Chien-Hung Lin, 林建宏
Other Authors: 蔡渙良
Format: Others
Language:zh-TW
Published: 2004
Online Access:http://ndltd.ncl.edu.tw/handle/33592240741984642557
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spelling ndltd-TW-091CCIT04280792016-06-24T04:15:32Z http://ndltd.ncl.edu.tw/handle/33592240741984642557 運用奇異線性指數二次高斯及迴路轉移函數回歸法從事傾斜轉彎自動駕儀之設計研究 Chien-Hung Lin 林建宏 碩士 國防大學中正理工學院 電子工程研究所 91 In this thesis, a bank-to-turn missile autopilot is designed by using the Generalized Singular Linear Exponential Quadratic Gaussian and Loop Transfer Recovery techniques. The Generalized Singular Linear Exponential Quadratic Gaussian method is adopted for two reasons. The first reason is that the process noise and measurement noise are considered in the system design so the robustness of the system is preserved. The second reason is this method can overcome the limitation in controller design of the Generalized Singular Linear Quadratic technique. Finally, numerical simulation results show that the Roll-Pitch-Yaw aerodynamic cross-coupling problems are solved and the stability of the system is also enhanced. 蔡渙良 陳功 2004 學位論文 ; thesis 0 zh-TW
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language zh-TW
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description 碩士 === 國防大學中正理工學院 === 電子工程研究所 === 91 === In this thesis, a bank-to-turn missile autopilot is designed by using the Generalized Singular Linear Exponential Quadratic Gaussian and Loop Transfer Recovery techniques. The Generalized Singular Linear Exponential Quadratic Gaussian method is adopted for two reasons. The first reason is that the process noise and measurement noise are considered in the system design so the robustness of the system is preserved. The second reason is this method can overcome the limitation in controller design of the Generalized Singular Linear Quadratic technique. Finally, numerical simulation results show that the Roll-Pitch-Yaw aerodynamic cross-coupling problems are solved and the stability of the system is also enhanced.
author2 蔡渙良
author_facet 蔡渙良
Chien-Hung Lin
林建宏
author Chien-Hung Lin
林建宏
spellingShingle Chien-Hung Lin
林建宏
運用奇異線性指數二次高斯及迴路轉移函數回歸法從事傾斜轉彎自動駕儀之設計研究
author_sort Chien-Hung Lin
title 運用奇異線性指數二次高斯及迴路轉移函數回歸法從事傾斜轉彎自動駕儀之設計研究
title_short 運用奇異線性指數二次高斯及迴路轉移函數回歸法從事傾斜轉彎自動駕儀之設計研究
title_full 運用奇異線性指數二次高斯及迴路轉移函數回歸法從事傾斜轉彎自動駕儀之設計研究
title_fullStr 運用奇異線性指數二次高斯及迴路轉移函數回歸法從事傾斜轉彎自動駕儀之設計研究
title_full_unstemmed 運用奇異線性指數二次高斯及迴路轉移函數回歸法從事傾斜轉彎自動駕儀之設計研究
title_sort 運用奇異線性指數二次高斯及迴路轉移函數回歸法從事傾斜轉彎自動駕儀之設計研究
publishDate 2004
url http://ndltd.ncl.edu.tw/handle/33592240741984642557
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