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dc.contributor.advisorRuss Tedrake.en_US
dc.contributor.authorMoore, Joseph L. (Joseph Lawrence)en_US
dc.contributor.otherMassachusetts Institute of Technology. Dept. of Mechanical Engineering.en_US
dc.date.accessioned2011-12-09T21:35:56Z
dc.date.available2011-12-09T21:35:56Z
dc.date.copyright2011en_US
dc.date.issued2011en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/67629
dc.descriptionThesis (S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2011.en_US
dc.descriptionCataloged from PDF version of thesis.en_US
dc.descriptionIncludes bibliographical references (p. 109-112).en_US
dc.description.abstractSmall and micro UAVs have enabled a number of new mission capabilities, including navigating in and around buildings and performing perch-and-stare surveillance. However, one of the primary limitations of these small vehicles is endurance, simply because they cannot carry sufficient power for long missions. Recent advances in fixed-wing perching have made it possible to consider a new solution to this problem - landing on a powerline to recharge. Furthermore, because a current carrying conductor generates a magnetic field, a unique opportunity exists to use the powerline not just for recharging, but for localization as well. In this thesis, we seek to develop technologies that will enable a fixed-wing aircraft to land on a powerline using only the powerline's magnetic field and an inertial measurement unit for localization. To achieve this goal, an experimental set-up and preliminary sensing hardware are developed to detect the magnetic field at least 4 meters from the wire. Then, the necessary signal processing and state estimation algorithms are applied to achieve successful localization and overcome problematic field ambiguities. Following this, an onboard sensing system is developed and the high speed tracking of a perching trajectory is demonstrated experimentally. Finally, the position error associated with the aircraft tracking algorithm is analyzed carefully and assessed to be suitable for achieving closed loop perching. The work culminates in a light weight, 30 gram, on-board sensor system with the capability of estimating the position of a perching aircraft in real time at update rates up to 320 Hz, positional accuracies ranging from 2 to 20 centimeters, and delays of about 17 Ms.en_US
dc.description.statementofresponsibilityby Joseph L. Moore.en_US
dc.format.extent112 p.en_US
dc.language.isoengen_US
dc.publisherMassachusetts Institute of Technologyen_US
dc.rightsM.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission.en_US
dc.rights.urihttp://dspace.mit.edu/handle/1721.1/7582en_US
dc.subjectMechanical Engineering.en_US
dc.titlePowerline perching with a fixed-wing UAVen_US
dc.typeThesisen_US
dc.description.degreeS.M.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Mechanical Engineering
dc.identifier.oclc765993896en_US


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