System Identification of Unmanned Helicopter: Applications to R-90

碩士 === 淡江大學 === 航空太空工程學系博士班 === 95 === The development of a parameterized model for a small-scale unmanned helicopter “H-ling” (a Thunder Tiger Raptor-90) and its identification using a frequency domain identification technique are described in this thesis. The construction of the R-90 dynamics usin...

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Main Authors: Jen-Hung Tseng, 曾仁宏
Other Authors: FU-YUEN HSIAO
Format: Others
Language:en_US
Published: 2007
Online Access:http://ndltd.ncl.edu.tw/handle/85597508275134117370
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spelling ndltd-TW-095TKU052950052015-10-13T14:08:16Z http://ndltd.ncl.edu.tw/handle/85597508275134117370 System Identification of Unmanned Helicopter: Applications to R-90 無人直昇機之系統鑑別應用於R90直昇機 Jen-Hung Tseng 曾仁宏 碩士 淡江大學 航空太空工程學系博士班 95 The development of a parameterized model for a small-scale unmanned helicopter “H-ling” (a Thunder Tiger Raptor-90) and its identification using a frequency domain identification technique are described in this thesis. The construction of the R-90 dynamics using system ID techniques in this work is for potential applications to the control of autonomous hovering. Taking into consideration the future controller design, we adopt transfer functions of main channels as our dynamics model that explicitly accounts for the stabilizer bar, which has a strong influence on the flight dynamics characteristics. Several algorithms and software are utilized to investigate this problem. In specific, we first adopt ARX as the primary identification algorithm, whose applicability has been verified with the Yamaha R-50 parameters. Results obtained from ARX are then cross-checked with those from CIFER and PEM. Numerical simulations are given to demonstrate the validity of our results. The ultimate goal of this investigation is to extend the current work to build a fully functional autonomous rotorcraft. FU-YUEN HSIAO 蕭富元 2007 學位論文 ; thesis 50 en_US
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description 碩士 === 淡江大學 === 航空太空工程學系博士班 === 95 === The development of a parameterized model for a small-scale unmanned helicopter “H-ling” (a Thunder Tiger Raptor-90) and its identification using a frequency domain identification technique are described in this thesis. The construction of the R-90 dynamics using system ID techniques in this work is for potential applications to the control of autonomous hovering. Taking into consideration the future controller design, we adopt transfer functions of main channels as our dynamics model that explicitly accounts for the stabilizer bar, which has a strong influence on the flight dynamics characteristics. Several algorithms and software are utilized to investigate this problem. In specific, we first adopt ARX as the primary identification algorithm, whose applicability has been verified with the Yamaha R-50 parameters. Results obtained from ARX are then cross-checked with those from CIFER and PEM. Numerical simulations are given to demonstrate the validity of our results. The ultimate goal of this investigation is to extend the current work to build a fully functional autonomous rotorcraft.
author2 FU-YUEN HSIAO
author_facet FU-YUEN HSIAO
Jen-Hung Tseng
曾仁宏
author Jen-Hung Tseng
曾仁宏
spellingShingle Jen-Hung Tseng
曾仁宏
System Identification of Unmanned Helicopter: Applications to R-90
author_sort Jen-Hung Tseng
title System Identification of Unmanned Helicopter: Applications to R-90
title_short System Identification of Unmanned Helicopter: Applications to R-90
title_full System Identification of Unmanned Helicopter: Applications to R-90
title_fullStr System Identification of Unmanned Helicopter: Applications to R-90
title_full_unstemmed System Identification of Unmanned Helicopter: Applications to R-90
title_sort system identification of unmanned helicopter: applications to r-90
publishDate 2007
url http://ndltd.ncl.edu.tw/handle/85597508275134117370
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