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dc.contributor.authorRoberts, John William
dc.contributor.authorCory, Rick
dc.contributor.authorTedrake, Russell Louis
dc.date.accessioned2010-12-01T18:26:32Z
dc.date.available2010-12-01T18:26:32Z
dc.date.issued2009-07
dc.date.submitted2009-06
dc.identifier.isbn978-1-4244-4523-3
dc.identifier.issn0743-1619
dc.identifier.otherINSPEC Accession Number: 10775903
dc.identifier.urihttp://hdl.handle.net/1721.1/60046
dc.description.abstractThe ability of birds to perch robustly and effectively is a powerful demonstration of the capabilities of nature's control systems. Their apparent robustness to gust disturbances is particularly remarkable because when the airspeed approaches zero just before acquiring a perch, the influence of aerodynamic forces, and therefore potentially the control authority, is severely compromised. In this paper we present a simplified closed-form model for a fixed-wing aircraft which closely agrees with experimental indoor perching data. We then carefully examine the LTV controllability along an optimized perching trajectory for three different actuation scenarios - a glider (no powerplant), a fixed propeller, and a propeller with thrust vectoring. The results reveal that while all three vehicles are LTV controllable along the trajectory, the additional actuators allow the perch to be more easily acquired with less control surface deflections. However, in all three cases, disturbances experienced just before reaching the perch cannot be effectively rejected.en_US
dc.description.sponsorshipNational Science Foundation (U.S.). Graduate Fellowship Programen_US
dc.description.sponsorshipMicrosoft Research. New Faculty Fellowship programen_US
dc.language.isoen_US
dc.publisherInstitute of Electrical and Electronics Engineersen_US
dc.relation.isversionofhttp://dx.doi.org/10.1109/ACC.2009.5160526en_US
dc.rightsArticle is made available in accordance with the publisher's policy and may be subject to US copyright law. Please refer to the publisher's site for terms of use.en_US
dc.sourceIEEEen_US
dc.titleOn the controllability of fixed-wing perchingen_US
dc.typeArticleen_US
dc.identifier.citationRoberts, J.W., R. Cory, and R. Tedrake. “On the controllability of fixed-wing perching.” American Control Conference, 2009. ACC '09. 2009. 2018-2023. © Copyright 2009 IEEEen_US
dc.contributor.departmentMassachusetts Institute of Technology. Computer Science and Artificial Intelligence Laboratoryen_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Electrical Engineering and Computer Scienceen_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Mechanical Engineeringen_US
dc.contributor.approverTedrake, Russell Louis
dc.contributor.mitauthorRoberts, John William
dc.contributor.mitauthorCory, Rick
dc.contributor.mitauthorTedrake, Russell Louis
dc.relation.journalProceedings of the American Control Conference, 2009en_US
dc.eprint.versionFinal published versionen_US
dc.type.urihttp://purl.org/eprint/type/ConferencePaperen_US
eprint.statushttp://purl.org/eprint/status/PeerRevieweden_US
dspace.orderedauthorsRoberts, John W.; Cory, Rick; Tedrake, Russen
dc.identifier.orcidhttps://orcid.org/0000-0002-8712-7092
mit.licensePUBLISHER_POLICYen_US
mit.metadata.statusComplete


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