Autopilot Design of a BTT Missile with a Front Lateral Jet to Enhance the Output Transient Responses

碩士 === 國立臺灣大學 === 電機工程學研究所 === 91 === In this thesis, a bank-to-turn autopilot design method is studied for a tail-controlled missile with a front lateral jet. The six degrees-of-freedom dynamical model of a short-range missile is described first. Then the linearization technique and lin...

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Main Authors: Liang-Yen Wang, 王良彥
Other Authors: I-Kong Fong
Format: Others
Language:zh-TW
Published: 2003
Online Access:http://ndltd.ncl.edu.tw/handle/26595024847914685397
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spelling ndltd-TW-091NTU004421042016-06-20T04:15:46Z http://ndltd.ncl.edu.tw/handle/26595024847914685397 Autopilot Design of a BTT Missile with a Front Lateral Jet to Enhance the Output Transient Responses 具彈頭側噴流之傾斜轉彎飛彈自動駕駛儀設計及其暫態改善 Liang-Yen Wang 王良彥 碩士 國立臺灣大學 電機工程學研究所 91 In this thesis, a bank-to-turn autopilot design method is studied for a tail-controlled missile with a front lateral jet. The six degrees-of-freedom dynamical model of a short-range missile is described first. Then the linearization technique and linear control theory are used for this autopilot design, with the goal of tracking input commands precisely. The quality of the output transient responses is also emphasized. Performance of the designed autopilot is demonstrated using nonlinear simulations. The front lateral jet system of the missile can produce large lateral force and a higher attack angle instantaneously so that the missile can turn quickly and have higher maneuverability. The simulation results of the present study do show the benefit of the front lateral jet. It is hoped that this preliminary study adequately demonstrates the performance potential of a missile with a lateral jet, and exposes the issues requiring further investigations. I-Kong Fong 馮蟻剛 2003 學位論文 ; thesis 76 zh-TW
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language zh-TW
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description 碩士 === 國立臺灣大學 === 電機工程學研究所 === 91 === In this thesis, a bank-to-turn autopilot design method is studied for a tail-controlled missile with a front lateral jet. The six degrees-of-freedom dynamical model of a short-range missile is described first. Then the linearization technique and linear control theory are used for this autopilot design, with the goal of tracking input commands precisely. The quality of the output transient responses is also emphasized. Performance of the designed autopilot is demonstrated using nonlinear simulations. The front lateral jet system of the missile can produce large lateral force and a higher attack angle instantaneously so that the missile can turn quickly and have higher maneuverability. The simulation results of the present study do show the benefit of the front lateral jet. It is hoped that this preliminary study adequately demonstrates the performance potential of a missile with a lateral jet, and exposes the issues requiring further investigations.
author2 I-Kong Fong
author_facet I-Kong Fong
Liang-Yen Wang
王良彥
author Liang-Yen Wang
王良彥
spellingShingle Liang-Yen Wang
王良彥
Autopilot Design of a BTT Missile with a Front Lateral Jet to Enhance the Output Transient Responses
author_sort Liang-Yen Wang
title Autopilot Design of a BTT Missile with a Front Lateral Jet to Enhance the Output Transient Responses
title_short Autopilot Design of a BTT Missile with a Front Lateral Jet to Enhance the Output Transient Responses
title_full Autopilot Design of a BTT Missile with a Front Lateral Jet to Enhance the Output Transient Responses
title_fullStr Autopilot Design of a BTT Missile with a Front Lateral Jet to Enhance the Output Transient Responses
title_full_unstemmed Autopilot Design of a BTT Missile with a Front Lateral Jet to Enhance the Output Transient Responses
title_sort autopilot design of a btt missile with a front lateral jet to enhance the output transient responses
publishDate 2003
url http://ndltd.ncl.edu.tw/handle/26595024847914685397
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