Altitude Control of Flapping-wing MAV

碩士 === 淡江大學 === 航空太空工程學系碩士班 === 98 === The trajectory control of flapping-wing microaerial vehicles (MAVs) is discussed in this paper. The Tamkang University (TKU) has been devoted to the development of flapping-wing robots for a long period, including design, fabrication and control. On the basis o...

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Main Authors: Sen-Huang Lin, 林森煌
Other Authors: 蕭富元
Format: Others
Language:zh-TW
Published: 2010
Online Access:http://ndltd.ncl.edu.tw/handle/57130373356452879021
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spelling ndltd-TW-098TKU052950072015-10-13T13:40:01Z http://ndltd.ncl.edu.tw/handle/57130373356452879021 Altitude Control of Flapping-wing MAV 微型拍翼機高度控制 Sen-Huang Lin 林森煌 碩士 淡江大學 航空太空工程學系碩士班 98 The trajectory control of flapping-wing microaerial vehicles (MAVs) is discussed in this paper. The Tamkang University (TKU) has been devoted to the development of flapping-wing robots for a long period, including design, fabrication and control. On the basis of the earlier knowledge on the Golden Snitch, a flapping-wing MAV in TKU, we develop a non- intrusive navigation methodology by using stereo vision, and stabilize the flight trajectory with a modified Pcontrol. Different from other mechanical or aerial systems, the selections in control signal are limited in this problem due to the restrictions in carry-on weight. Numerical simulations also provided to demonstrate the robustness of our control law, and flight test is used to examine this design. From the experiment results we have demonstrated the feasibility of our algorithm. 蕭富元 2010 學位論文 ; thesis 55 zh-TW
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description 碩士 === 淡江大學 === 航空太空工程學系碩士班 === 98 === The trajectory control of flapping-wing microaerial vehicles (MAVs) is discussed in this paper. The Tamkang University (TKU) has been devoted to the development of flapping-wing robots for a long period, including design, fabrication and control. On the basis of the earlier knowledge on the Golden Snitch, a flapping-wing MAV in TKU, we develop a non- intrusive navigation methodology by using stereo vision, and stabilize the flight trajectory with a modified Pcontrol. Different from other mechanical or aerial systems, the selections in control signal are limited in this problem due to the restrictions in carry-on weight. Numerical simulations also provided to demonstrate the robustness of our control law, and flight test is used to examine this design. From the experiment results we have demonstrated the feasibility of our algorithm.
author2 蕭富元
author_facet 蕭富元
Sen-Huang Lin
林森煌
author Sen-Huang Lin
林森煌
spellingShingle Sen-Huang Lin
林森煌
Altitude Control of Flapping-wing MAV
author_sort Sen-Huang Lin
title Altitude Control of Flapping-wing MAV
title_short Altitude Control of Flapping-wing MAV
title_full Altitude Control of Flapping-wing MAV
title_fullStr Altitude Control of Flapping-wing MAV
title_full_unstemmed Altitude Control of Flapping-wing MAV
title_sort altitude control of flapping-wing mav
publishDate 2010
url http://ndltd.ncl.edu.tw/handle/57130373356452879021
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