Matches in SemOpenAlex for { <https://semopenalex.org/work/W4313148421> ?p ?o ?g. }
Showing items 1 to 71 of
71
with 100 items per page.
- W4313148421 abstract "Through the efforts of robotic engineers and inspired by the flapping flight of smaller creatures (e.g., insects and hummingbirds), the untethered stable hovering of flapping micro-aerial vehicles (FMAVs) has been achieved. Now, engineers are evaluating how to improve the mobility of these vehicles. The maneuverability of insects and birds in flight, such as their sharp turns and their takeoffs and landings from vertical walls, is what researchers originally expected from FMAVs. However, in previous studies, just one active (or one active plus one passive) degree of freedom (DoF) was given to the main actuation of the wing, and the range of movement of the wings was small. In addition, the magnitude of the attitude control torque that could be generated was relatively small when compared with multi-rotors. However, with the recent developments of small motors and drive-circuit technology, the realization of untethered flight by FMAVs equipped with four or more motors seems possible. This study utilized numerical calculation to investigate the advantage of a flapping-flight robot equipped with two pairs of left and right wings capable of stroke and twisting movements with two independent DoFs ( <tex xmlns:mml=http://www.w3.org/1998/Math/MathML xmlns:xlink=http://www.w3.org/1999/xlink>$2times 2$</tex> -DoF FMAV). The results of the numerical studies confirmed that, compared with the split-factor method widely used in past studies, the <tex xmlns:mml=http://www.w3.org/1998/Math/MathML xmlns:xlink=http://www.w3.org/1999/xlink>$2times 2$</tex> -DoF FMAV can generate higher yaw torque without the need for additional large driving torque. This shows that various agile flight functions are possible." @default.
- W4313148421 created "2023-01-06" @default.
- W4313148421 creator A5012455392 @default.
- W4313148421 date "2022-10-23" @default.
- W4313148421 modified "2023-10-16" @default.
- W4313148421 title "Toward Dexterous Flapping Flight: Effective Large Yaw Torque Generation by $2times 2$-Degrees-of-Freedom Flapping Wings" @default.
- W4313148421 cites W114595877 @default.
- W4313148421 cites W1963636759 @default.
- W4313148421 cites W1965705114 @default.
- W4313148421 cites W1968475932 @default.
- W4313148421 cites W1969142892 @default.
- W4313148421 cites W2029976533 @default.
- W4313148421 cites W2072035469 @default.
- W4313148421 cites W2074190841 @default.
- W4313148421 cites W2107093838 @default.
- W4313148421 cites W2114338873 @default.
- W4313148421 cites W2158532293 @default.
- W4313148421 cites W2332654577 @default.
- W4313148421 cites W2955102412 @default.
- W4313148421 cites W3007998343 @default.
- W4313148421 cites W3109900720 @default.
- W4313148421 doi "https://doi.org/10.1109/iros47612.2022.9981990" @default.
- W4313148421 hasPublicationYear "2022" @default.
- W4313148421 type Work @default.
- W4313148421 citedByCount "0" @default.
- W4313148421 crossrefType "proceedings-article" @default.
- W4313148421 hasAuthorship W4313148421A5012455392 @default.
- W4313148421 hasConcept C121332964 @default.
- W4313148421 hasConcept C127413603 @default.
- W4313148421 hasConcept C13393347 @default.
- W4313148421 hasConcept C144171764 @default.
- W4313148421 hasConcept C146978453 @default.
- W4313148421 hasConcept C155710575 @default.
- W4313148421 hasConcept C206923515 @default.
- W4313148421 hasConcept C208081375 @default.
- W4313148421 hasConcept C2780444116 @default.
- W4313148421 hasConcept C41008148 @default.
- W4313148421 hasConcept C44154836 @default.
- W4313148421 hasConcept C62520636 @default.
- W4313148421 hasConcept C97257150 @default.
- W4313148421 hasConcept C97355855 @default.
- W4313148421 hasConceptScore W4313148421C121332964 @default.
- W4313148421 hasConceptScore W4313148421C127413603 @default.
- W4313148421 hasConceptScore W4313148421C13393347 @default.
- W4313148421 hasConceptScore W4313148421C144171764 @default.
- W4313148421 hasConceptScore W4313148421C146978453 @default.
- W4313148421 hasConceptScore W4313148421C155710575 @default.
- W4313148421 hasConceptScore W4313148421C206923515 @default.
- W4313148421 hasConceptScore W4313148421C208081375 @default.
- W4313148421 hasConceptScore W4313148421C2780444116 @default.
- W4313148421 hasConceptScore W4313148421C41008148 @default.
- W4313148421 hasConceptScore W4313148421C44154836 @default.
- W4313148421 hasConceptScore W4313148421C62520636 @default.
- W4313148421 hasConceptScore W4313148421C97257150 @default.
- W4313148421 hasConceptScore W4313148421C97355855 @default.
- W4313148421 hasLocation W43131484211 @default.
- W4313148421 hasOpenAccess W4313148421 @default.
- W4313148421 hasPrimaryLocation W43131484211 @default.
- W4313148421 hasRelatedWork W2003778936 @default.
- W4313148421 hasRelatedWork W2324986161 @default.
- W4313148421 hasRelatedWork W2471259897 @default.
- W4313148421 hasRelatedWork W2519606573 @default.
- W4313148421 hasRelatedWork W2576311655 @default.
- W4313148421 hasRelatedWork W296902894 @default.
- W4313148421 hasRelatedWork W3159712780 @default.
- W4313148421 hasRelatedWork W4205954251 @default.
- W4313148421 hasRelatedWork W4230151801 @default.
- W4313148421 hasRelatedWork W4378188455 @default.
- W4313148421 isParatext "false" @default.
- W4313148421 isRetracted "false" @default.
- W4313148421 workType "article" @default.