Please use this identifier to cite or link to this item:
http://arks.princeton.edu/ark:/88435/dsp01h989r596p
Full metadata record
DC Field | Value | Language |
---|---|---|
dc.contributor.advisor | Rowley, Clarence | - |
dc.contributor.advisor | Majumdar, Anirudha | - |
dc.contributor.author | Lynch, Grace | - |
dc.contributor.author | Sudhakar, Soumya | - |
dc.date.accessioned | 2018-08-20T14:20:59Z | - |
dc.date.available | 2018-08-20T14:20:59Z | - |
dc.date.created | 2018-05-02 | - |
dc.date.issued | 2018-08-20 | - |
dc.identifier.uri | http://arks.princeton.edu/ark:/88435/dsp01h989r596p | - |
dc.description.abstract | The goal of this project is to design an off board control, sensing and computation system that will allow a fixed-wing unmanned aerial vehicle (UAV) to transition autonomously from forward flight to vertical hover in a maneuver called propeller-hang. The capability to transition to prop-hang autonomously will allow the UAV to avoid obstacles and operate in a safer manner. A communication loop was created using Vicon motion capture equipment and a modified remote controlled UAV for off-board sensing. Control algorithms and observers were tested in simulation and in experiments, with transition to prop-hang successful, though with poor control in φ and y. The best LQR controller was one that was less aggressive while the finite difference reconstruction working the best for state estimation. | en_US |
dc.format.mimetype | application/pdf | - |
dc.language.iso | en | en_US |
dc.title | Control of Propeller Hang on Fixed Wing UAV | en_US |
dc.type | Princeton University Senior Theses | - |
pu.date.classyear | 2018 | en_US |
pu.department | Mechanical and Aerospace Engineering | en_US |
pu.pdf.coverpage | SeniorThesisCoverPage | - |
pu.contributor.authorid | 960915422 | - |
pu.certificate | Robotics & Intelligent Systems Program | en_US |
Appears in Collections: | Mechanical and Aerospace Engineering, 1924-2019 |
Files in This Item:
File | Description | Size | Format | |
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LYNCH-GRACE-THESIS-etal.pdf | 18.93 MB | Adobe PDF | Request a copy |
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