Robust H_infinity Control of Tracking Systems with Time-Varying Uncertainties

碩士 === 國立高雄應用科技大學 === 機械與精密工程研究所 === 99 === This thesis proposes a robust control approach for tracking systems with time-varying uncertainties. First, weighting functions for loop shaping are chosen to combine with the original system such that a generalized plant is formed. Then, for the general...

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Main Authors: Yi-Sheng Luo, 羅易聖
Other Authors: Liang-An Zheng
Format: Others
Language:zh-TW
Published: 100
Online Access:http://ndltd.ncl.edu.tw/handle/18640377675244466127
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spelling ndltd-TW-099KUAS86930652015-10-16T04:02:47Z http://ndltd.ncl.edu.tw/handle/18640377675244466127 Robust H_infinity Control of Tracking Systems with Time-Varying Uncertainties 具時變不確定量追蹤系統之H_infinity強健控制 Yi-Sheng Luo 羅易聖 碩士 國立高雄應用科技大學 機械與精密工程研究所 99 This thesis proposes a robust control approach for tracking systems with time-varying uncertainties. First, weighting functions for loop shaping are chosen to combine with the original system such that a generalized plant is formed. Then, for the generalized plant, a controller is obtained by using control method. The Hybrid Taguchi-Genetic Algorithm (HTGA) is employed to find the optimal gains of the weighting functions which will lead to a stabilizing controller. Then, a sufficient condition in terms of linear matrix inequalities (LMIs) is employed to guarantee that the resulting control tracking system is asymptotically stable in the presence of time-varying uncertainties. Finally, a simulation of a missile autopilot system is given to demonstrate the use of the design approach. The results show that the designed missile system can efficiently track the reference input and ensure its stability in the presence of time-varying uncertainties. Liang-An Zheng 鄭良安 100 學位論文 ; thesis 67 zh-TW
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language zh-TW
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description 碩士 === 國立高雄應用科技大學 === 機械與精密工程研究所 === 99 === This thesis proposes a robust control approach for tracking systems with time-varying uncertainties. First, weighting functions for loop shaping are chosen to combine with the original system such that a generalized plant is formed. Then, for the generalized plant, a controller is obtained by using control method. The Hybrid Taguchi-Genetic Algorithm (HTGA) is employed to find the optimal gains of the weighting functions which will lead to a stabilizing controller. Then, a sufficient condition in terms of linear matrix inequalities (LMIs) is employed to guarantee that the resulting control tracking system is asymptotically stable in the presence of time-varying uncertainties. Finally, a simulation of a missile autopilot system is given to demonstrate the use of the design approach. The results show that the designed missile system can efficiently track the reference input and ensure its stability in the presence of time-varying uncertainties.
author2 Liang-An Zheng
author_facet Liang-An Zheng
Yi-Sheng Luo
羅易聖
author Yi-Sheng Luo
羅易聖
spellingShingle Yi-Sheng Luo
羅易聖
Robust H_infinity Control of Tracking Systems with Time-Varying Uncertainties
author_sort Yi-Sheng Luo
title Robust H_infinity Control of Tracking Systems with Time-Varying Uncertainties
title_short Robust H_infinity Control of Tracking Systems with Time-Varying Uncertainties
title_full Robust H_infinity Control of Tracking Systems with Time-Varying Uncertainties
title_fullStr Robust H_infinity Control of Tracking Systems with Time-Varying Uncertainties
title_full_unstemmed Robust H_infinity Control of Tracking Systems with Time-Varying Uncertainties
title_sort robust h_infinity control of tracking systems with time-varying uncertainties
publishDate 100
url http://ndltd.ncl.edu.tw/handle/18640377675244466127
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AT luóyìshèng jùshíbiànbùquèdìngliàngzhuīzōngxìtǒngzhīhinfinityqiángjiànkòngzhì
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