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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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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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.
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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 |
work_keys_str_mv |
AT senhuanglin altitudecontrolofflappingwingmav AT línsēnhuáng altitudecontrolofflappingwingmav AT senhuanglin wēixíngpāiyìjīgāodùkòngzhì AT línsēnhuáng wēixíngpāiyìjīgāodùkòngzhì |
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