Energetics-based design of small flapping-wing micro air vehicles
In this paper, the energetics of a flapping-wing micro air vehicle (MAV) is analyzed with the objective of designing it. The salient features of this paper are as follows: 1) designing an energy storage mechanism in the air vehicle similar to an insect thorax that stores part of the kinetic energy o...
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| Veröffentlicht in: | IEEE/ASME transactions on mechatronics 2006-08, Vol.11 (4), p.433-438 |
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| container_title | IEEE/ASME transactions on mechatronics |
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| creator | Madangopal, R. Zaeem Ashraf Khan Agrawal, S.K. |
| description | In this paper, the energetics of a flapping-wing micro air vehicle (MAV) is analyzed with the objective of designing it. The salient features of this paper are as follows: 1) designing an energy storage mechanism in the air vehicle similar to an insect thorax that stores part of the kinetic energy of the wing as elastic potential energy during a flapping cycle; 2) inclusion of simplified aerodynamic wing models and inertia of the mechanism using rigid-body modeling techniques; 3) optimization of parameters of the energy storage mechanism using the dynamic models, so that energy input from the external actuators is minimized during a flapping cycle. A series of engineering prototypes based on these studies have been planned which will justify the use of these mathematical techniques |
| doi_str_mv | 10.1109/TMECH.2006.878525 |
| format | Article |
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The salient features of this paper are as follows: 1) designing an energy storage mechanism in the air vehicle similar to an insect thorax that stores part of the kinetic energy of the wing as elastic potential energy during a flapping cycle; 2) inclusion of simplified aerodynamic wing models and inertia of the mechanism using rigid-body modeling techniques; 3) optimization of parameters of the energy storage mechanism using the dynamic models, so that energy input from the external actuators is minimized during a flapping cycle. A series of engineering prototypes based on these studies have been planned which will justify the use of these mathematical techniques</description><identifier>ISSN: 1083-4435</identifier><identifier>EISSN: 1941-014X</identifier><identifier>DOI: 10.1109/TMECH.2006.878525</identifier><identifier>CODEN: IATEFW</identifier><language>eng</language><publisher>New York: IEEE</publisher><subject>Actuators ; Aerodynamics ; Design ; Design engineering ; Design optimization ; energetics ; Energy storage ; Flapping ; flapping wing machines ; Inclusions ; Insects ; Kinetic energy ; Mathematical models ; Mechatronics ; Micro air vehicles ; Potential energy ; Stores ; Thorax ; Vehicle dynamics ; Wings (aircraft)</subject><ispartof>IEEE/ASME transactions on mechatronics, 2006-08, Vol.11 (4), p.433-438</ispartof><rights>Copyright The Institute of Electrical and Electronics Engineers, Inc. (IEEE) 2006</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c391t-17e94aef82cabeaa1bc763e8d0427d3fdc7d36a7f987dee1af7f8b8ba59ef1393</citedby><cites>FETCH-LOGICAL-c391t-17e94aef82cabeaa1bc763e8d0427d3fdc7d36a7f987dee1af7f8b8ba59ef1393</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://ieeexplore.ieee.org/document/1677575$$EHTML$$P50$$Gieee$$H</linktohtml><link.rule.ids>314,776,780,792,27903,27904,54736</link.rule.ids><linktorsrc>$$Uhttps://ieeexplore.ieee.org/document/1677575$$EView_record_in_IEEE$$FView_record_in_$$GIEEE</linktorsrc></links><search><creatorcontrib>Madangopal, R.</creatorcontrib><creatorcontrib>Zaeem Ashraf Khan</creatorcontrib><creatorcontrib>Agrawal, S.K.</creatorcontrib><title>Energetics-based design of small flapping-wing micro air vehicles</title><title>IEEE/ASME transactions on mechatronics</title><addtitle>TMECH</addtitle><description>In this paper, the energetics of a flapping-wing micro air vehicle (MAV) is analyzed with the objective of designing it. 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A series of engineering prototypes based on these studies have been planned which will justify the use of these mathematical techniques</description><subject>Actuators</subject><subject>Aerodynamics</subject><subject>Design</subject><subject>Design engineering</subject><subject>Design optimization</subject><subject>energetics</subject><subject>Energy storage</subject><subject>Flapping</subject><subject>flapping wing machines</subject><subject>Inclusions</subject><subject>Insects</subject><subject>Kinetic energy</subject><subject>Mathematical models</subject><subject>Mechatronics</subject><subject>Micro air vehicles</subject><subject>Potential energy</subject><subject>Stores</subject><subject>Thorax</subject><subject>Vehicle dynamics</subject><subject>Wings (aircraft)</subject><issn>1083-4435</issn><issn>1941-014X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2006</creationdate><recordtype>article</recordtype><sourceid>RIE</sourceid><recordid>eNpdkE1LAzEQhoMoWKs_QLwsnrxszWySTXIspVpB8VLBW8juTmrKfpm0iv_erSsIXmbm8LzDzEPIJdAZANW366flYjXLKM1nSiqRiSMyAc0hpcBfj4eZKpZyzsQpOYtxSynlQGFC5ssWwwZ3voxpYSNWSYXRb9qkc0lsbF0nrrZ979tN-jmUpPFl6BLrQ_KBb76sMZ6TE2friBe_fUpe7pbrxSp9fL5_WMwf05Jp2KUgUXOLTmWlLdBaKEqZM1QV5ZmsmKvKoeZWOq1khQjWSacKVVih0QHTbEpuxr196N73GHem8bHEurYtdvtoIJeQsYzqA3r9D912-9AO1xmVCwmcCj5AMELDQzEGdKYPvrHhywA1B6fmx6k5ODWj0yFzNWY8Iv7xuZRCCvYNYC1zNA</recordid><startdate>20060801</startdate><enddate>20060801</enddate><creator>Madangopal, R.</creator><creator>Zaeem Ashraf Khan</creator><creator>Agrawal, S.K.</creator><general>IEEE</general><general>The Institute of Electrical and Electronics Engineers, Inc. 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The salient features of this paper are as follows: 1) designing an energy storage mechanism in the air vehicle similar to an insect thorax that stores part of the kinetic energy of the wing as elastic potential energy during a flapping cycle; 2) inclusion of simplified aerodynamic wing models and inertia of the mechanism using rigid-body modeling techniques; 3) optimization of parameters of the energy storage mechanism using the dynamic models, so that energy input from the external actuators is minimized during a flapping cycle. A series of engineering prototypes based on these studies have been planned which will justify the use of these mathematical techniques</abstract><cop>New York</cop><pub>IEEE</pub><doi>10.1109/TMECH.2006.878525</doi><tpages>6</tpages></addata></record> |
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| language | eng |
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| source | IEEE Electronic Library (IEL) |
| subjects | Actuators Aerodynamics Design Design engineering Design optimization energetics Energy storage Flapping flapping wing machines Inclusions Insects Kinetic energy Mathematical models Mechatronics Micro air vehicles Potential energy Stores Thorax Vehicle dynamics Wings (aircraft) |
| title | Energetics-based design of small flapping-wing micro air vehicles |
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