F-16 Lateral Auto-pilot Command0generator Tracker Design by the Integration of H2/H∞ Method

碩士 === 中華大學 === 電機工程學系 === 86 ===   This dissertation presents the F-16 lateral auto-pilot Command Generator Tracker (CGT) designed by the Linear Exponential Quadrati aussian with Loop Transfer rECOVERY (LEQG/LTR) methodology. The LEQG/LTR optimal controller, providing additional parameter "Q&q...

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Main Authors: Lu, Yung-Nan, 呂永南
Other Authors: Hwang, Chi-Kuang
Format: Others
Language:zh-TW
Published: 1998
Online Access:http://ndltd.ncl.edu.tw/handle/69888808289207709390
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spelling ndltd-TW-086CHPI34420012016-01-22T04:17:04Z http://ndltd.ncl.edu.tw/handle/69888808289207709390 F-16 Lateral Auto-pilot Command0generator Tracker Design by the Integration of H2/H∞ Method 利用「H2」及「H∞」整合型方式設計F-16戰鬥機側向自動駕駛機 Lu, Yung-Nan 呂永南 碩士 中華大學 電機工程學系 86   This dissertation presents the F-16 lateral auto-pilot Command Generator Tracker (CGT) designed by the Linear Exponential Quadrati aussian with Loop Transfer rECOVERY (LEQG/LTR) methodology. The LEQG/LTR optimal controller, providing additional parameter "Q" for the control input weightimg matrix, consists of both state-feedback and feedforward controllers. Based on the original state weighting matrix "Q" and control input weighting matrix "R", the additional parameter provides a systematic adjustment is in the cross terms of the control input weighting martix "R" which is the less sense for us to select. If the positive value of the parameter "Q" is selected, we can improve the high gain problem with increasing the effective control input weighting matrix R. The performance of the system may be even better because of the cross terms of the matrix R. AII the time-domain, frequency-domain and robust design techniques are unified into one design procedure which is derived in this dissertation Applying the procedure to both methods, the performance of LEQG/LTR method is better than that of the traditional Linear Quadratic Gaussian with Loop Transfer Recovery (LQG/LTR)   Owing to some restrictions of using the LQG/LTR and LEQG/LTR methods, we propose and present the integration of H2/H methodology This method is a powerful method for designing the robust multivariable feedback control system. The optimal controller, consisting of both H2 and H synthesis theory, utilizes the H2 synthesis as a first cut to get a sense for what level of performance is achievable. The H synthesis theory, with its performance criterion based on the outcome of the first cut H2 design, is used to do the final work. The integration of H2/H methodology can combine the good properties of using H2 or H synthesis theory individually. Hwang, Chi-Kuang 黃啟光 1998 學位論文 ; thesis 67 zh-TW
collection NDLTD
language zh-TW
format Others
sources NDLTD
description 碩士 === 中華大學 === 電機工程學系 === 86 ===   This dissertation presents the F-16 lateral auto-pilot Command Generator Tracker (CGT) designed by the Linear Exponential Quadrati aussian with Loop Transfer rECOVERY (LEQG/LTR) methodology. The LEQG/LTR optimal controller, providing additional parameter "Q" for the control input weightimg matrix, consists of both state-feedback and feedforward controllers. Based on the original state weighting matrix "Q" and control input weighting matrix "R", the additional parameter provides a systematic adjustment is in the cross terms of the control input weighting martix "R" which is the less sense for us to select. If the positive value of the parameter "Q" is selected, we can improve the high gain problem with increasing the effective control input weighting matrix R. The performance of the system may be even better because of the cross terms of the matrix R. AII the time-domain, frequency-domain and robust design techniques are unified into one design procedure which is derived in this dissertation Applying the procedure to both methods, the performance of LEQG/LTR method is better than that of the traditional Linear Quadratic Gaussian with Loop Transfer Recovery (LQG/LTR)   Owing to some restrictions of using the LQG/LTR and LEQG/LTR methods, we propose and present the integration of H2/H methodology This method is a powerful method for designing the robust multivariable feedback control system. The optimal controller, consisting of both H2 and H synthesis theory, utilizes the H2 synthesis as a first cut to get a sense for what level of performance is achievable. The H synthesis theory, with its performance criterion based on the outcome of the first cut H2 design, is used to do the final work. The integration of H2/H methodology can combine the good properties of using H2 or H synthesis theory individually.
author2 Hwang, Chi-Kuang
author_facet Hwang, Chi-Kuang
Lu, Yung-Nan
呂永南
author Lu, Yung-Nan
呂永南
spellingShingle Lu, Yung-Nan
呂永南
F-16 Lateral Auto-pilot Command0generator Tracker Design by the Integration of H2/H∞ Method
author_sort Lu, Yung-Nan
title F-16 Lateral Auto-pilot Command0generator Tracker Design by the Integration of H2/H∞ Method
title_short F-16 Lateral Auto-pilot Command0generator Tracker Design by the Integration of H2/H∞ Method
title_full F-16 Lateral Auto-pilot Command0generator Tracker Design by the Integration of H2/H∞ Method
title_fullStr F-16 Lateral Auto-pilot Command0generator Tracker Design by the Integration of H2/H∞ Method
title_full_unstemmed F-16 Lateral Auto-pilot Command0generator Tracker Design by the Integration of H2/H∞ Method
title_sort f-16 lateral auto-pilot command0generator tracker design by the integration of h2/h∞ method
publishDate 1998
url http://ndltd.ncl.edu.tw/handle/69888808289207709390
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