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dc.contributor.advisorJohn J. Deyst.en_US
dc.contributor.authorToohey, Damianen_US
dc.contributor.otherMassachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.en_US
dc.date.accessioned2006-03-29T18:46:17Z
dc.date.available2006-03-29T18:46:17Z
dc.date.issued2005en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/32457
dc.descriptionThesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2005.en_US
dc.description"June 2005."en_US
dc.descriptionIncludes bibliographical references (leaf 84).en_US
dc.description.abstractThe goal of the MIT Draper Partnership Program is to develop a system capable of deploying a cluster of ISR (intelligence, surveillance, reconnaissance) sensors over an area of interest. One of the proposed methods is a guided parafoil vehicle that is deployed from a UAV. After unfurling its canopy, it is envisioned that the vehicle would follow a planned trajectory to the target, and vision-based targeting system would be employed to provide the necessary accuracy. A 6DOF parafoil simulation was created in the Matlab/Simulink environment to study the parafoil dynamics and assess the feasibility of the delivery method. The parafoil's range and controllability were tested under a variety of simulated wind conditions, and a hypothetical mission was conceived to evaluate the performance of the proposed trajectory designs and guidance laws. Also, an extended Kalman filter was incorporated into the simulation to determine effectiveness of the camera-based targeting system and other navigation sensors.en_US
dc.description.statementofresponsibilityby Damian Toohey.en_US
dc.format.extent91 leavesen_US
dc.format.extent3705741 bytes
dc.format.extent3710104 bytes
dc.format.mimetypeapplication/pdf
dc.format.mimetypeapplication/pdf
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/1721.1/7582
dc.subjectAeronautics and Astronautics.en_US
dc.titleDevelopment of a small parafoil vehicle for precision deliveryen_US
dc.typeThesisen_US
dc.description.degreeS.M.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc61751396en_US


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