Project Archive
Persistent link for this collectionhttps://hdl.handle.net/11299/163581
Included is an archive of previous research projects at the UAV Laboratories. These archives should provide insight into the research performed, data associated with the research, and any analysis scripts to parse and interpret the data.
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Item Ultra Stick 120 Motor Mount(2014-07-23) Glasheen, KatherineItem UAV for Reliability Senior Design Project(2014-07-23) Bergquist, Erik; Reimann, Shawn; Amos, Jeremy; Cole, Jay; Phillips, Justin; Shuster, SimonItem ACC 2013, An Airborne Experimental Test Platform: From Theory to Flight Companion Software Package(2014-07-23) Dorobantu, AndreiItem Goldy Flight Control System v1.0(2014-07-23) Johnson, WillItem Rate Table Characterization of Analog Devices ADIS 16405 and Vector Nav VN 100 Inertial Measurement Units(2014-07-23) Taylor, BrianItem Sensor Integration Software(2014-07-23) Murch, AustinItem UAV Laboratories Processes and Procedures(2014-07-23) Taylor, BrianItem Image Navigation UROP Research(2014-07-23) VandenAvond, SeanItem Python Attitude Heading and Reference System(2014-07-23) Taylor, BrianItem ACC 2014, Structural Model Identification of a Small Flexible Aircraft Companion Software Package(2014-07-23) Moreno, ClaudiaItem AMSYS Instructions(2014-07-24) Layh, TrevorItem MPC5200B Daughterboard Design(2014-07-24) Murch, AustinItem Cell Phone Navigation(2015-02) Layh, Trevor; Larson, Jordan; Jackson, John; Agamawi, Yunus; Taylor, Brian; Gebre-Egziabher, Demoz; Krause, Joel; Gustafson, JacobCell Phone Navigation project funded by the U.S. Department of Homeland Security in Fall 2013 which tasked the UMN UAV Research Lab with proposing a backup navigation system within one year for SUAVs in GPS-denied environments. A cascaded Attitude Heading Reference System and Dead Reckoning system was designed which was capable of being aided by cell phone time-of-arrival information. This backup navigation system was integrated into a UltraStick 25e airframe equipped with the Goldy Flight Control System. Flight testing was conducted to characterize performance during short duration GPS outages. Longer duration GPS outages were simulated using Monte Carlo hardware-in-the-loop simulations. A full report on this work was created for DHS and is included in this project archive. Additionally, this research was presented and published for the Institute of Navigation International Technical Meeting, and those materials are also included in this project archive.