關鍵字查詢 | 類別:會議論文 | | 關鍵字:MAV

[第一頁][上頁]12[次頁][最末頁]目前在第 1 頁 / 共有 43 筆查詢結果
序號 學年期 教師動態
1 108/1 機械系 楊龍杰 教授 會議論文 發佈 Wing rotation FWMAV using servos , [108-1] :Wing rotation FWMAV using servos會議論文Wing rotation FWMAV using servosNikhil Panchal; Kompala Saravana; Reshmi Waikhom; Lung-Jieh Yang; Wei He; Yuan-Lung Loen_US國際無20190827~20190829Yang, Lung-Jieh是CHNICIUS 2019Beijing, China
2 108/1 機械系 楊龍杰 教授 會議論文 發佈 Design of a wing rotation mechanism for a FWMAV , [108-1] :Design of a wing rotation mechanism for a FWMAV會議論文Design of a wing rotation mechanism for a FWMAVSaravana Kompala; Nikhil Panchal; Lung-Jieh Yang; Balasubramanian Esakki; Sarasu Packiriswamyen_US國際無20190827~20190829Yang, Lung-Jieh是CHNICIUS 2019Beijing, China
3 99/2 航太系 洪健君 副教授 會議論文 發佈 Optimization Approach on Flapping Aerodynamic Characteristics of Corrugated Airfoil , [99-2] :Optimization Approach on Flapping Aerodynamic Characteristics of Corrugated Airfoil會議論文Optimization Approach on Flapping Aerodynamic Characteristics of Corrugated AirfoilSun, W.-H; Miao, J-.M; Tai, C.-H; Hung, C.-C.MAVs;aerodynamic,;ANOVA analysis; vorticityMY74000The development of biomimetic micro-aerial-vehicles (MAVs) with flapping wings is the future trend in military/domestic field. The successful flight of MAVs is strongly related to the understanding of unsteady aerodynamic performance of low Reynolds number airfoils under dynamic flapping motion. This study explored the effects of flapping frequency, stroke amplitude, and the inclined angle of stroke plane on lift force and thrust force of a bio-inspiration corrugated airfoil with 33 full factorial design of experiment and ANOVA analysis. Unsteady vorticity flows over a corrugated thin airfoil executing flapping motion are computed with time-dependent two-dimensional laminar incompressible Reynolds-averaged Navier-S
4 106/2 機電系 楊龍杰 教授 會議論文 發佈 The development of flapping micro air vehicle Golden-Snitch at TKU Taiwan , [106-2] :The development of flapping micro air vehicle Golden-Snitch at TKU Taiwan會議論文The development of flapping micro air vehicle Golden-Snitch at TKU TaiwanLung-Jieh YangProceeding of ICAME 2018Flapping wing micro air vehicles (FWMAVs) or ornithopters have several advantages compared with rotary and fixed wings because of their maneuverable, high power efficiency at low speed flight and durable. The invited talk presents the development of FWMAVs of 20 cm span and total weight less than 15 gram at Tamkang University, Taiwan. The real manufacture of several prototypes as well as their wind tunnel force measurement and numerical simulations are performed with flapping stroke angles of 53° and 90°, in diverse wind velocities ranging between 1-3 m/sec, and with flapping frequencies about 14-15 Hz. Some technical issues including autonomous flight control, avionics miniaturization, 3D flow simulation, and flow visualization will be also addressed.en國際無20180322~20180324是INDICAME 2018Chennai, India
5 106/2 機電系 楊龍杰 教授 會議論文 發佈 Numerical and Experimental Verifications on the Wing Design of a Flapping Wing Micro Air Vehicle , [106-2] :Numerical and Experimental Verifications on the Wing Design of a Flapping Wing Micro Air Vehicle會議論文Numerical and Experimental Verifications on the Wing Design of a Flapping Wing Micro Air VehicleLung-Jieh YangOrnithopter;Flapping Wing;Micro Air Vehicle (MAV);Fluid-Structural Interaction (FSI)Proceeding of IDAD 2018This talk is to demonstrate the numerical and experimental verifications on the modified wing design of a flapping wing micro air vehicles (FWMAVs). The subject is a flapping wing of 20 cm span used in micro ornithopters subject to the conditions of 13-15 Hz flapping, inclined body angle of 20 degrees and the upwind speed of 0-3 m/s. In the first part, numerical simulations will be performed through varying the density of mesh for half flapping wing profile with wind tunnel domain for varied flapping stroke angles 53° and 90°. Comparative evaluation of 3D numerical and experimental lift force data relevant to the translational and rotational lift phenomenon’s of Dickinson’s
6 106/1 機電系 楊龍杰 教授 會議論文 發佈 Preliminary study on altitude and heading control of FWMAVs , [106-1] :Preliminary study on altitude and heading control of FWMAVs會議論文Preliminary study on altitude and heading control of FWMAVsN. Panchal; L.J. Yang; X. Zhang; B. EsakkiProc. of ICIUS 2017en國際淡水校園20170821~20170824L.J. Yang是TWNICIUS 2017Tamsui, Taiwan
7 106/1 機電系 楊龍杰 教授 會議論文 發佈 Image Processing Framework towards motion estimation and control of multiple FWMAVs , [106-1] :Image Processing Framework towards motion estimation and control of multiple FWMAVs會議論文Image Processing Framework towards motion estimation and control of multiple FWMAVsSankarasrinivasan S.; B. Esakki; L.J. YangProc. of ICIUS 2017en國際淡水校園20170821~20170824Sankarasrinivasan S.是TWNICIUS 2017Tamsui, Taiwan
8 105/2 機電系 楊龍杰 教授 會議論文 發佈 Arduino-Based Autonomous Flight Control of FWMAVS , [105-2] :Arduino-Based Autonomous Flight Control of FWMAVS會議論文Arduino-Based Autonomous Flight Control of FWMAVSLung-Jieh Yang; Suseendar Marimuthu; Yow-Ting Lin; Balasubramanian EsakkiProc. of the 1st International Conference on Engineering and Science (ICES 2016)en國內無20170709~20170711Lung-Jieh Yang是TWNThe 1st International Conference on Engineering and Science (ICES 2016)Ilan, Taiwan
9 105/1 機電系 楊龍杰 教授 會議論文 發佈 An Arduino-Based IMU/MCU for 15-gram Flapping Wing MAVs , [105-1] :An Arduino-Based IMU/MCU for 15-gram Flapping Wing MAVs會議論文An Arduino-Based IMU/MCU for 15-gram Flapping Wing MAVsL.-J. Yang, S. Marimuthu; Y.-T. LinProc. of ICIUS 2016en國內無20160822~20160825L.-J. Yang是CHNThe 12th International Conference on Intelligent Unmanned Systems (ICIUS 2016)Xian, China
10 103/2 機電系 楊龍杰 教授 會議論文 發佈 Robust Vision Based Target Tracking Algorithm for MAV Navigation System , [103-2] :Robust Vision Based Target Tracking Algorithm for MAV Navigation System會議論文Robust Vision Based Target Tracking Algorithm for MAV Navigation SystemSankarasrinivasan S; Balasubramanian E; Hsiao Fu-Yuen; Yang Lung-JiehProc. of ICIC 2015en_US國際無20150528~20150530Balasubramanian E是INDInternational Conference on Industrial Instrumentation & Control (ICIC 2015)Pune, Maharashtra, India
11 104/1 機電系 楊龍杰 教授 會議論文 發佈 Re-STOL Micro Ornithopters- with 4 Improvement Strategies , [104-1] :Re-STOL Micro Ornithopters- with 4 Improvement Strategies會議論文Re-STOL Micro Ornithopters- with 4 Improvement StrategiesL.J. Yang; C.W. Chen; H.H. Ke; Y.T. Lin; S. Marimuthu; K.C. Hungornithopter;repeatable STOL;PV-charging;Arduino-based;flapping mechanismProc. of ICIUS 2015Regarding to the 20-cm wingspan flapping micro-air-vehicles (MAVs) or ornithopters, how to prolong the operation time and improve the flight control is very critical to their roadmap of development. Based on using the available technology and commercial transducer devices, this work presents four new features of ornithopters and proves them feasible. The 1st feature is repeatable short take-off and landing (re-STOL) so that the ornithopter can stop flapping in the air and automatically falls on the ground with resetting to the good gesture of take-off. The 2nd feature is to recharge the onboard Lithium battery by flexible photo-voltaic (PV) thin film on the tail. Recharging can be done either during flight or on the g
12 101/1 航太系 蕭富元 副教授 會議論文 發佈 New flapping mechanisms of MAV Golden Snitch , [101-1] :New flapping mechanisms of MAV Golden Snitch會議論文New flapping mechanisms of MAV Golden Snitch楊龍杰; Cheng, Chieh-Ming ; Chiang, Yi-Wei; Hsiao, Fu-Yuan淡江大學機械與機電工程學系; 淡江大學航空太空工程學系SIM UniversityThe 8th International Conference on Intelligent Unmanned Systems (ICIUS 2012)tku_id: 000096520; 000126120;Submitted by 龍杰 楊 (ljyang@mail.tku.edu.tw) on 2012-12-11T06:13:00Z No. of bitstreams: 1 NO-016_Full manuscript_submission template_ICIUS2012.doc: 734720 bytes, checksum: 5182681246b1a44011cac34f7d268eb5 (MD5);Made available in DSpace on 2012-12-11T06:13:01Z (GMT). No. of bitstreams: 1 NO-016_Full manuscript_submission template_ICIUS2012.doc: 734720 bytes, checksum: 5182681246b1a44011cac34f7d268eb5 (MD5)en國際20121022~20121024楊龍杰YSGPThe 8th International Conference on Intelligent Unmanned Systems (ICIUS 2012)Singapore<links><record><name>機構典藏連結</name><url>http://tkuir.lib.tku.edu.tw:8080/dspace/handle/987654321/79554</url></record></links>
13 101/1 航太系 蕭富元 副教授 會議論文 發佈 「淡江金探子」拍翼機之研製 , [101-1] :「淡江金探子」拍翼機之研製會議論文「淡江金探子」拍翼機之研製楊龍杰; Yang, Lung-jieh; 蕭富元; Hsiao, Fu-yuen; 馮朝剛淡江大學機械與機電工程學系; 淡江大學航空太空工程學系拍翼飛行機器人;雙拍翼升力延遲;八字拍翼;Flapping micro air vehicle (MAV);lift lag of the flapping wing pair, figure-of-8中國:北京航空航天大學第八屆海峽兩岸航空太空學術研討會論文集北京航空航天大學航空科學與工程學院本文回顧淡江大學自2003年以來發展之「淡江金探子」拍翼機研製歷程。「淡江金探子」翼展20公分,總質量10克以下,使用可充電式鋰聚合物電池提供電動馬達所需電力,帶動拍翼機構運行,並採用遙控方式操作,一次充電可連續飛行8分鐘,目前適用於航空科普推廣教育與競賽之實作教具。本文也描述了「淡江金探子」的概念設計、研發瓶頸與相關學術成果。This paper presents the developing of Tamkang’s flapping micro air vehicle (MAV) named as “Golden Snitch” since 2003. “Golden Snitch” has a wingspan of 20 cm and a total body mass of 10 gram. It used polylithium battery to provide the electricity required to the flapping mechanism operation. With one full charging of the battery “Golden Snitch” could fly for 8 min under the wireless remote control and therefore is appropriate to the popular science applications. The authors also addressed the concept design of the f lapping MAV, the difficulty encountered during the research an
14 101/1 航太系 馮朝剛 教授 會議論文 發佈 「淡江金探子」拍翼機之研製 , [101-1] :「淡江金探子」拍翼機之研製會議論文「淡江金探子」拍翼機之研製楊龍杰; Yang, Lung-jieh; 蕭富元; Hsiao, Fu-yuen; 馮朝剛淡江大學機械與機電工程學系; 淡江大學航空太空工程學系拍翼飛行機器人;雙拍翼升力延遲;八字拍翼;Flapping micro air vehicle (MAV);lift lag of the flapping wing pair, figure-of-8中國:北京航空航天大學第八屆海峽兩岸航空太空學術研討會論文集北京航空航天大學航空科學與工程學院本文回顧淡江大學自2003年以來發展之「淡江金探子」拍翼機研製歷程。「淡江金探子」翼展20公分,總質量10克以下,使用可充電式鋰聚合物電池提供電動馬達所需電力,帶動拍翼機構運行,並採用遙控方式操作,一次充電可連續飛行8分鐘,目前適用於航空科普推廣教育與競賽之實作教具。本文也描述了「淡江金探子」的概念設計、研發瓶頸與相關學術成果。This paper presents the developing of Tamkang’s flapping micro air vehicle (MAV) named as “Golden Snitch” since 2003. “Golden Snitch” has a wingspan of 20 cm and a total body mass of 10 gram. It used polylithium battery to provide the electricity required to the flapping mechanism operation. With one full charging of the battery “Golden Snitch” could fly for 8 min under the wireless remote control and therefore is appropriate to the popular science applications. The authors also addressed the concept design of the f lapping MAV, the difficulty encountered during the research an
15 93/2 機電系 楊龍杰 教授 會議論文 發佈 The micro aerial vehicle (MAV) with flapping wings , [93-2] :The micro aerial vehicle (MAV) with flapping wings會議論文The micro aerial vehicle (MAV) with flapping wings楊龍杰; Yang, Lung-jieh; Hsu, Cheng-kuei; Ho, Jen-yang; Wang, Hsin-hsiung; Feng, Gwo-hwa淡江大學機械與機電工程學系N.Y.: IEEE (Institute of Electrical and Electronic Engineers)ICM '05. IEEE International Conference on Mechatronics, Taipei, pp.811-815The research of micro aerial vehicles (MAVs) is a new field of low-Reynolds-number flow, which attracts much attention in the advanced aeronautical area. The flapping wing, proved by many natural flyers, is the most appropriate way of flying objects which sizes are less than 6 inches. However, there is still plenty of room for studying on the unsteady aerodynamic characteristics of flapping wings. The flapping wing, which is light weighted and high strengthened, is originally composed of the titanium-alloy frame and the parylene skin. Such an integration of fabrication needs the help of MEMS processing. Additionally, the flapping test after the wing fabri
16 96/2 機電系 楊龍杰 教授 會議論文 發佈 Surface Tension-Driven Micro Actuator to Micro Aerial Vehicles (MAVS) , [96-2] :Surface Tension-Driven Micro Actuator to Micro Aerial Vehicles (MAVS)會議論文Surface Tension-Driven Micro Actuator to Micro Aerial Vehicles (MAVS)Huang, J.; Kao, C. Y.; Yang, L. J.淡江大學機械與機電工程學系Surface tension;Micro aerial vehicleProceedings of the 4th Asia Pacific Conference on Transducers and Micro-Nano Technologies (APCOT 2008),4p.National Cheng Kung University (NCKU)This paper describes a novel micro actuator that adopts surface tension as the driving force. The concept, design, and fabrication were discussed in this work. This device regards a SU-8 peacock-like microstructure as the prototype. After modifying this original peacock-like microstructure, we supposed a novel idea of mounting this surface tension actuator to the tail of a flapping micro aerial vehicle (MAV) and control the flight attitude.tku_id: 000096520;Submitted by 數位組工讀生 (deer+std@mail.tku.edu.tw) on 2014-03-07T03:38:41Z No. of bitstreams: 0;Made available in DSpace on 2014-03-07T03:38:42Z (GMT). No. of b
17 96/1 機電系 楊龍杰 教授 會議論文 發佈 拍撲式微飛行器之減重設計及其空氣動力性能調校研究 , [96-1] :拍撲式微飛行器之減重設計及其空氣動力性能調校研究會議論文拍撲式微飛行器之減重設計及其空氣動力性能調校研究The Study on the Reduction Weight of Flapping MAV and Adjusting it's Aerodynamic Performance高敏維; 施宏明; 徐振貴; 楊龍杰淡江大學機械與機電工程學系輕量化;微飛行器;齒輪傳動系統;Reducing weight;MAV;Transmission system;PVDF;Parylene2007中華民國航空太空學會第四十九屆航太學術研討會論文集,6頁教育部為了讓微飛行器有足夠的升力及推力,輕量化是微飛行器研究的首要課題。本研究成功選擇不同的材料如塑膠、鋁等高強度的材料進行馬達基座等零組件的減重,並搭配上由國外購得之質輕齒輪及管徑更小的中空管,使齒輪傳動系統的部份達到輕量化,並讓微飛行器成功飛行15 秒以上。此外,為了能更精確的調校微飛行器之空氣動力特性,本文也提出以一嶄新的智慧型機翼,探討拍撲式微飛行器之空氣動力特性。此研究特別指定拍撲翼之右翼翼膜為聚對二甲苯(parylene),左翼翼膜為聚對二甲苯與PVDF(polyvinylidene fluoride)之複合機翼。在風洞測試時,左翼之PVDF 感應器可直接獲得左翼之升力訊號,整個微飛行器之升力訊號則由多軸力規擷取,此種機翼設計構型可輕易找出左翼及右翼個別之升力貢獻。本研究即利用此方法並微調兩翼間拍撲運動的相位差,來調校拍撲式微飛行器之空氣動力特性。;In order to make the Micro Aerial Vehicle (MAV) having sufficient lift and thrust, reduce the weight of the MAV is the main subject of this article. Here we show the different choice in materials, such as plastic and aluminum, and we had successfully miniaturized the framework of the motor assembly. We combine light gears bought f
18 96/2 機電系 楊龍杰 教授 會議論文 發佈 拍翼式微飛行器之設計及改良 , [96-2] :拍翼式微飛行器之設計及改良會議論文拍翼式微飛行器之設計及改良The Design and Improvement of the Flapping Micro Aerial Vehicles房柏廷; 黃奕澄; 高崇瑜; 楊龍杰; 沈永康淡江大學機械與機電工程學系拍翼式微飛行器;聚對二甲苯;輕量化;塑膠模組2008TGPD玩具與遊戲設計暨造形設計研討會論文集 08'=Proceedings of Toy, Game, and Plastic Design (TGPD),8頁臺北教育大學本文所研究之拍翼式微飛行器,利用四連桿機構,結合減速齒輪組,配合外購之馬達、無線模組晶片、鋰電池,從第一代鈦合金機翼骨架與聚對二甲苯(parylene)之薄膜機翼延伸至第二代壓克力基座和巴沙木機翼骨架,最後第三代拍翼式微飛行器改成輕量化之全鋁連桿基座和碳纖維機翼骨架,並持續改良各項機構之設計,最後製作出總重量約6克之拍翼式微飛行器Micro Aerial Vehicle(MAV),經由實際試飛也能穩定之飛行。此外,也利用風洞實驗去探討微飛行器之空氣動力特性,經由數據與試飛找出微飛行器之最佳化設計。而全塑膠模組化將結合模具量產技術,最後以商品化方式呈現,具有輕量化、彈性化之優勢,且降低成本提高製作效率。本研究團隊未來也將持續精進改善,為拍翼式微飛行器增加其研究價值。tku_id: ; 000096520;Submitted by 數位組工讀生 (deer+std@mail.tku.edu.tw) on 2014-03-07T03:42:18Z No. of bitstreams: 0;Made available in DSpace on 2014-03-07T03:42:19Z (GMT). No. of bitstreams: 0zh_TW國際20080606~20080606TWN2008TGPD玩具與遊戲設計暨造形設計研討會=2008 Conference of Toy, Game, and Plastic Design (TGPD)臺北市, 臺灣<links><record><name>機構典藏連結</name><url>http://tkuir.lib.tku.edu.tw:8080/dspace/handle/987654321/96450</url
19 96/1 機電系 楊龍杰 教授 會議論文 發佈 可撓機翼架構誘導之仿生八字形拍翼 , [96-1] :可撓機翼架構誘導之仿生八字形拍翼會議論文可撓機翼架構誘導之仿生八字形拍翼A Biomimic Figure-Eight Flapping Induced by Flexible Wing Frames徐振貴; 施宏明; 楊龍杰淡江大學機械與機電工程學系拍翼;微飛行器;八字形;Flapping;Micro aerial vehicle (MAV);Figure-eight2007中華民國航空太空學會第四十九屆航太學術研討會論文集,6頁教育部有別於傳統的拍翼機構為剛性的認定,本研究提議使用可撓式的碳纖維棒與聚對二甲苯薄膜,分別作為掌狀大小微飛行器之機翼骨架與機翼蒙皮。即便拍翼(齒輪連桿)傳動機構只是單自由度的四連桿(機構)設計,但上下拍翼的連動經由可撓性機翼的材質與外型設計,成功耦合到流向的前後振動,故使翼尖組合出三維的八字形拍翼軌跡。該八字形軌跡以高速攝影機成功拍攝驗證,且發生於接近或甚至超過18Hz 的拍翼頻率,本仿生機翼應用於全機重10gw 以下,翼展20cm 以下的拍翼微飛行器,已可持續飛行32 秒以上。飛行測試結果顯示,本仿生八字形拍翼軌跡可經由空氣彈性力學之本質而自動產生,無需藉助複雜精巧的三維機構設計。;Relaxing from the conventional regarding of the "rigid" flapping mechanism, in this work the authors proposed to use the "flexible" carbon-fibers and parylene films as the wing frames for palm-size micro aerial vehicles (MAVs). By combining the coupling streamwise vibration of the wing frame and the driving flapping motion with one degree of freedom only, a figure-eight stroke of wing tips trajectory is verified via a high speed camera with the flapping frequency beyond 18 H
20 96/2 機電系 楊龍杰 教授 會議論文 發佈 A Biomimetic Figure-of-Eight Flapping of Micro Aerial Vehicles (MAVS) Illuminated by LEDs , [96-2] :A Biomimetic Figure-of-Eight Flapping of Micro Aerial Vehicles (MAVS) Illuminated by LEDs會議論文A Biomimetic Figure-of-Eight Flapping of Micro Aerial Vehicles (MAVS) Illuminated by LEDsYang, Lung-Jieh; Kao, Min-Wei; Hsu, Chen-Kuei; Liao, Chun-Wei; Huang, I-Cheng; Fang, Pai-Ting淡江大學機械與機電工程學系MAV;LED;Figure-of-eightProceedings of the 4th Asia Pacific Conference on Transducers and Micro-Nano Technologies (APCOT 2008),4p.National Cheng Kung University (NCKU)This article presents a method of using LEDs on the wing tip of a flapping MAV (Micro Aerial Vehicle) for observing the wing tip trajectory. In general, the wing tip trajectory is recorded by a high speed CCD due to the higher flapping frequency. However, using high speed CCDs is not convenient because the equipment is heavy and not portable. In order to overcome this problem, this work installed LEDs on the wing tip of our flapping MAV. And then the images of the wing tip trajectory can be recorded by usual digital video camaras (DV). Fina
21 95/1 機電系 楊龍杰 教授 會議論文 發佈 拍撲式微型飛行系統之研製(I) , [95-1] :拍撲式微型飛行系統之研製(I)會議論文拍撲式微型飛行系統之研製(I)Research on Fabrication of Flapping Micro Aerial Vehicles (I)楊龍杰; 王信雄; 劉冠君; 徐振貴; 馮國華;施宏明淡江大學機械與機電工程學系微飛行器;拍撲翼;現地量測;微機電系統;壓電;Micro aerial vehicle (MAV);Flapping wing;On-site measurement;Micro-electro-mechanical system (MEMS);Piezoelectric國科會自動化學門九十四年度專題計畫成果發表會暨學門規劃研討會論文集,6頁淡江大學本研究以拍撲式微飛行器之實際升空飛行為研究目標。基於以往計畫執行所得之微飛行器製作技術加以精進,在本計畫前段利用微機電技術來完成飛行器之自主飛行測試,飛行距離已可達10公尺。同時借重多維度的測力設備,得出本微飛行器之空氣動力特性,包含升力係數與推力係數等量測數據。為得到更好的飛行表現,改良現有傳動系統,並透過高性能且質輕之鋰電池、多功能質輕的複合式晶片之襄助來縮減重量,以及利用類似鳥類的尾翼設計,來大幅延長本微飛行器之滯空時間。改良後的微飛行器之無線遙控飛行時間已超過10秒,距離達40公尺以上。;The objective of this project is to develop a flapping MAV capable of flight via wireless control. Based on the previous fabricating experience of MAVs, we have a great progress in this year. The first half of the research result, we fabricated a MAV having a successful flight capability of 10-meter range by MEMS process. The aerodynamic forces of this MAV were also obtained by a multi-dimensional load-cell in the facility of th
22 96/1 機電系 徐振貴 技士 會議論文 發佈 可撓機翼架構誘導之仿生八字形拍翼 , [96-1] :可撓機翼架構誘導之仿生八字形拍翼會議論文可撓機翼架構誘導之仿生八字形拍翼A Biomimic Figure-Eight Flapping Induced by Flexible Wing Frames徐振貴; 施宏明; 楊龍杰淡江大學機械與機電工程學系拍翼;微飛行器;八字形;Flapping;Micro aerial vehicle (MAV);Figure-eight2007中華民國航空太空學會第四十九屆航太學術研討會論文集,6頁教育部有別於傳統的拍翼機構為剛性的認定,本研究提議使用可撓式的碳纖維棒與聚對二甲苯薄膜,分別作為掌狀大小微飛行器之機翼骨架與機翼蒙皮。即便拍翼(齒輪連桿)傳動機構只是單自由度的四連桿(機構)設計,但上下拍翼的連動經由可撓性機翼的材質與外型設計,成功耦合到流向的前後振動,故使翼尖組合出三維的八字形拍翼軌跡。該八字形軌跡以高速攝影機成功拍攝驗證,且發生於接近或甚至超過18Hz 的拍翼頻率,本仿生機翼應用於全機重10gw 以下,翼展20cm 以下的拍翼微飛行器,已可持續飛行32 秒以上。飛行測試結果顯示,本仿生八字形拍翼軌跡可經由空氣彈性力學之本質而自動產生,無需藉助複雜精巧的三維機構設計。;Relaxing from the conventional regarding of the "rigid" flapping mechanism, in this work the authors proposed to use the "flexible" carbon-fibers and parylene films as the wing frames for palm-size micro aerial vehicles (MAVs). By combining the coupling streamwise vibration of the wing frame and the driving flapping motion with one degree of freedom only, a figure-eight stroke of wing tips trajectory is verified via a high speed camera with the flapping frequency beyond 18 H
23 97/1 航太系 蕭富元 副教授 會議論文 發佈 精密射出成型於微飛行器零組件成形之研究 , [97-1] :精密射出成型於微飛行器零組件成形之研究會議論文精密射出成型於微飛行器零組件成形之研究Study on Fabrication of Micro Aerial Vehicle Parts by Precision Injection Molding沈永康; 黃進光; 楊龍杰; 蕭富元; 苗志銘; 李建邦; 鄧秉敦淡江大學機械與機電工程學系; 淡江大學航空太空工程學系精密射出成型;MAV ;模流分析;材料試驗;Precision Injection Molding;Micro Aerial Vehicle (MAV);Moldflow Analysis;Material Testing臺北市:中華民國航空太空學會中華民國航空太空學會第五十屆年會暨學術研討會國科會航太學門成果發表會會議首冊暨論文摘要集,頁155中華民國航空太空學會; 國科會工程科技推展中心本文的目的是以精密射出成型製作微飛行器零件,針對不同材料進行機械性質之分析。由於微飛行器各部份零件之功能需求有所不同,利用ASTM 標準,對兩種材料(POM ; PA66)進行磨耗; 拉伸與衝擊試驗,以作為微飛行器各部份零件材料選用之參考。結果顯示POM 之抗拉強度優於PA66 ;衝擊試驗中, POM 之衝擊強度優於PA66 ;磨耗試驗中, POM 之耐磨耗性質略高於PA66 '因此連桿,基座及齒輪選用POM 材料進行製作。本文針對精密射出成型做成型性之探討,並利用成型視窗找出田口法之參數,以田口實驗計劃法,找出影響微飛行器零件收縮之重要參數,並找出最佳化的製程參數。結果顯示,影響收縮最重要之製程參數依序為模具溫度; 射出壓力; 保壓時間,最後是熔膠溫度。三個零件之最佳化製程參數相同,皆為AIBIC3D3 '分別為模其溫度的。c ; :熔膠溫度220 0C ; 射出壓力500b訂以及保壓時間2 秒。;This investigation fabricates the parts of MAV(Micro Aerial Vehicle) by using precision injection molding.The authors use different polymer materials to do the material testing. The authors base on ASTM stand
24 97/1 航太系 蕭富元 副教授 會議論文 發佈 Dynamics of Flapping Micro-Aerial Vehicles , [97-1] :Dynamics of Flapping Micro-Aerial Vehicles會議論文Dynamics of Flapping Micro-Aerial Vehicles拍翼式微飛行器之動力學分析楊澤明; 蕭富元淡江大學航空太空工程學系Flapping wing;Micro aerial vehicles (MA Vs);Flight dynamics;Averaging Theory;拍撲翼;微型飛行器(MAVs) ;飛行動力學;平均理論臺北市:中華民國航空太空學會中華民國航空太空學會第五十屆年會暨學術研討會國科會航太學門成果發表會會議首冊暨論文摘要集,頁113中華民國航空太空學會; 國科會工程科技推展中心本文主要在探討拍翼式微型飛行器(MAVs)之動力學分析。此微型飛行器已由淡江大學微機電實驗室開發多年。藉由我們推導出的動力學模型,我們將與實飛的飛行數據做比較。雖然已有很多文獻討論過類似的議題,但在此篇論文中,我們利用實際的飛行數據來印證我們所推導的動力學模型以及假設之正確性。月時我們利用風洞測試的數據,求其平均之氣動力特性,因此我們可以利用分析定翼機的方法來討論拍翼式飛行器。藉由飛行數據與數值模擬的比較,證明了我們的動力學模型是正確的。;The dynamics of flapping wing micro aerial vehicles (MAVs) is studied in this paper. The MEMS Laboratory in Tamkang University has been developing flapping wing MAVs for several years. Based on the developed flapping wing MAV we study its dynamics and compare our results with flight test data. Although several papers have discussed similar topics previously, using our flight test data we demonstrate the validity of some assumptions and our derivations. We a
25 97/1 機電系 徐振貴 技士 會議論文 發佈 拍翼式飛行器之飛行測試及仿生式尾翼控制器之研製 , [97-1] :拍翼式飛行器之飛行測試及仿生式尾翼控制器之研製會議論文拍翼式飛行器之飛行測試及仿生式尾翼控制器之研製The flying test and the fabrication of a biomemitic tail controller of flapping MAVs (micro aerial vehicles)許政慶; 房柏廷; 黃奕澄; 高崇瑜; 廖俊瑋; 黃建博; 高敏維; 徐振貴; 楊龍杰淡江大學機械與機電工程學系拍翼式微飛行器;放電線切割;仿生;微機電製程;flapping MAV;EDWC;biomimetic;MEMS process臺北市:中華民國航空太空學會中華民國航空太空學會第五十屆年會暨學術研討會國科會航太學門成果發表會會議首冊暨論文摘要集,頁159中華民國航空太空學會; 國科會工程科技推展中心本研究以拍翼式微飛行器之設計、製造、測試與遙控飛行之整合為研究目標。本團隊過去曾成功利用減重之鋁製連桿與馬達機座組裝拍翼式微飛行器,並使其飛行32 秒。而本研究也將利用過去所用之微飛行器製作技術'開發性能更佳的拍翼式微飛行器。在本研究中,本團隊設計了更過合長時間飛行的連桿及馬達基座,而同樣如過去以放電線切割技術製作鋁製傳動機構連桿組,進行拍翼式微飛行器之組裝,並完成飛行器之遙控飛行測試。此外,本研究設計了新型的機身及尾翼架構,利用此種機身及尾翼飛行架構組裝之拍翼式微飛行器,飛行距離已可達到公尺,飛行高度達10公尺,飛行時間已可超過2分鐘。最後,本研究也參考過去本團隊所製造之仿生式微閥門,設計並以微機電製程製造微型致動器,預計以此致動器達到尾翼穩定控制的目標。;This research shows the design, fabrication, and test ofthe MAV (Micro Aerial Vehicle). Our group had ever used the EDWC (Electric Discharge Wire Cutting) technology to fabricate the light aluminum linkages and the motor base of the MAY. Then we assembled the MAV and flew it in the sky with 32 s
26 97/1 機電系 楊龍杰 教授 會議論文 發佈 精密射出成型於微飛行器零組件成形之研究 , [97-1] :精密射出成型於微飛行器零組件成形之研究會議論文精密射出成型於微飛行器零組件成形之研究Study on Fabrication of Micro Aerial Vehicle Parts by Precision Injection Molding沈永康; 黃進光; 楊龍杰; 蕭富元; 苗志銘; 李建邦; 鄧秉敦淡江大學機械與機電工程學系; 淡江大學航空太空工程學系精密射出成型;MAV ;模流分析;材料試驗;Precision Injection Molding;Micro Aerial Vehicle (MAV);Moldflow Analysis;Material Testing臺北市:中華民國航空太空學會中華民國航空太空學會第五十屆年會暨學術研討會國科會航太學門成果發表會會議首冊暨論文摘要集,頁155中華民國航空太空學會; 國科會工程科技推展中心本文的目的是以精密射出成型製作微飛行器零件,針對不同材料進行機械性質之分析。由於微飛行器各部份零件之功能需求有所不同,利用ASTM 標準,對兩種材料(POM ; PA66)進行磨耗; 拉伸與衝擊試驗,以作為微飛行器各部份零件材料選用之參考。結果顯示POM 之抗拉強度優於PA66 ;衝擊試驗中, POM 之衝擊強度優於PA66 ;磨耗試驗中, POM 之耐磨耗性質略高於PA66 '因此連桿,基座及齒輪選用POM 材料進行製作。本文針對精密射出成型做成型性之探討,並利用成型視窗找出田口法之參數,以田口實驗計劃法,找出影響微飛行器零件收縮之重要參數,並找出最佳化的製程參數。結果顯示,影響收縮最重要之製程參數依序為模具溫度; 射出壓力; 保壓時間,最後是熔膠溫度。三個零件之最佳化製程參數相同,皆為AIBIC3D3 '分別為模其溫度的。c ; :熔膠溫度220 0C ; 射出壓力500b訂以及保壓時間2 秒。;This investigation fabricates the parts of MAV(Micro Aerial Vehicle) by using precision injection molding.The authors use different polymer materials to do the material testing. The authors base on ASTM stand
27 97/1 機電系 楊龍杰 教授 會議論文 發佈 結合LED 之拍翼製作與其翼尖軌跡顯像技術 , [97-1] :結合LED 之拍翼製作與其翼尖軌跡顯像技術會議論文結合LED 之拍翼製作與其翼尖軌跡顯像技術A figure-of-eight flappiog recorded by LEDs on wingtip黃奕澄; 楊龍杰; 高敏維淡江大學機械與機電工程學系微飛行器;拍翼;發光二極體;8 字軌跡;MAV;flapping;light emission diode (LED);figure-of-eight trajectory臺北市:中華民國航空太空學會中華民國航空太空學會第五十屆年會暨學術研討會國科會航太學門成果發表會會議首冊暨論文摘要集,頁161中華民國航空太空學會; 國科會工程科技推展中心即時觀察拍翼式微型飛行器(MAV) 飛行時的翼尖軌跡,一般而言並不容易。尤對於MAV 較高之拍翼頻率,宜採用高速電荷搞合元件(CCD)攝影機錄製紀錄其翼尖軌跡,但由於高速CCD 設備沈重,不易攜帶,且高速CCD不便即時追蹤飛行路徑,即使追縱得了,也無法細部分辨MAV 各質點的姿態軌跡。為此,本研究特利用發光二極體(LED) 晶粒黏貼於拍翼式MAV 之翼尖,清楚直接用肉眼觀察到其翼尖亮點的軌跡'為一個傾斜的阿拉伯數字8。;The authors present a method for observing the wing tip trajectory a flapping micro aerial vehicle (MAV) In general the wing tip traectory is recorded by a high speed charge coupled device (CCD) due to the higher flapping frequency. However, using high speed CCDs is not convenient because the equipment is heavy and not portable. In order to overcome this problem, this work installed light emission diodes (LEDs) on the wing tip of our flapping MAY. And then the images of the wing
28 97/1 機電系 楊龍杰 教授 會議論文 發佈 拍翼式飛行器之飛行測試及仿生式尾翼控制器之研製 , [97-1] :拍翼式飛行器之飛行測試及仿生式尾翼控制器之研製會議論文拍翼式飛行器之飛行測試及仿生式尾翼控制器之研製The flying test and the fabrication of a biomemitic tail controller of flapping MAVs (micro aerial vehicles)許政慶; 房柏廷; 黃奕澄; 高崇瑜; 廖俊瑋; 黃建博; 高敏維; 徐振貴; 楊龍杰淡江大學機械與機電工程學系拍翼式微飛行器;放電線切割;仿生;微機電製程;flapping MAV;EDWC;biomimetic;MEMS process臺北市:中華民國航空太空學會中華民國航空太空學會第五十屆年會暨學術研討會國科會航太學門成果發表會會議首冊暨論文摘要集,頁159中華民國航空太空學會; 國科會工程科技推展中心本研究以拍翼式微飛行器之設計、製造、測試與遙控飛行之整合為研究目標。本團隊過去曾成功利用減重之鋁製連桿與馬達機座組裝拍翼式微飛行器,並使其飛行32 秒。而本研究也將利用過去所用之微飛行器製作技術'開發性能更佳的拍翼式微飛行器。在本研究中,本團隊設計了更過合長時間飛行的連桿及馬達基座,而同樣如過去以放電線切割技術製作鋁製傳動機構連桿組,進行拍翼式微飛行器之組裝,並完成飛行器之遙控飛行測試。此外,本研究設計了新型的機身及尾翼架構,利用此種機身及尾翼飛行架構組裝之拍翼式微飛行器,飛行距離已可達到公尺,飛行高度達10公尺,飛行時間已可超過2分鐘。最後,本研究也參考過去本團隊所製造之仿生式微閥門,設計並以微機電製程製造微型致動器,預計以此致動器達到尾翼穩定控制的目標。;This research shows the design, fabrication, and test ofthe MAV (Micro Aerial Vehicle). Our group had ever used the EDWC (Electric Discharge Wire Cutting) technology to fabricate the light aluminum linkages and the motor base of the MAY. Then we assembled the MAV and flew it in the sky with 32 s
29 102/1 機電系 楊龍杰 教授 會議論文 發佈 2D quasi-steady flow investigation of a flexible flapping wing , [102-1] :2D quasi-steady flow investigation of a flexible flapping wing會議論文2D quasi-steady flow investigation of a flexible flapping wingYang, L.-J.; Huang, H.-L.; Hung, K.-C.; Liou, J.-C.; Marimuthu, S.; Chandrasekhar, U.淡江大學機械與機電工程學系MAVThe 9th International Conference on Intelligent Unmanned Systems (ICIUS 2013), 4p.A 2D flow simulation of a flapping wing “Golden Snitch” with wing boundary fed from stereo-photography measurement is firstly conducted in this paper. The whole research framework is shown in Figure 1. Softwares Matlab, Surfer, and Gambit were used to slice a quarter-span cross section from the previous 3D trajectory of Figure 2 as the 2D solid boundary for the quasi-steady CFD simulation by Fluent. The time-varying outputs include the 2D flow fields in Figure 3 and the corresponding lift coefficient. The one cycle history of lift coefficient subject to 14 Hz flapping is qualitatively similar to the wind tunnel data.tku_id: 000096520;Submitted by 龍杰 楊 (ljyang@mail.tku.edu.tw
30 101/2 機電系 楊龍杰 教授 會議論文 發佈 Steel-based tail actuators for micro-air-vehicles , [101-2] :Steel-based tail actuators for micro-air-vehicles會議論文Steel-based tail actuators for micro-air-vehiclesYang, Lung-Jieh; Jan, Dung-Lin; Lin, Wei-Chung淡江大學機械與機電工程學系steel foil;tail actuator;laser cutting;micro-air-vehicles(MAVs)Institute of Electrical and Electronics Engineers ( IEEE )The 8th IEEE International Conference on Nano/Micro Engineered and Molecular Systems (IEEE NEMS 2013)Institute of Electrical and Electronics Engineers ( IEEE )This work presents an animation of the sporangial motion for making bionic tail flaps of micro-air-vehicles (MAVs) regarding energy saving. A SUS-304 steel foil of 40 μm-thick is used as the substrate and Nd-YAG laser cutting is performed to construct the surface tension-driven actuator. Surface modification including parylene coating and oxygen plasma treatment are tried to enlarge the actuation stroke angle.tku_id: 000096520;Submitted by 龍杰 楊 (ljyang@mail.tku.edu.tw) on 2013-12-07T02:20:18Z No. of bitstreams: 1 NEMS2013_paper_#107_MAV.pdf: 18
[第一頁][上頁]12[次頁][最末頁]目前在第 1 頁 / 共有 43 筆查詢結果