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- W3119389933 abstract "In other works, it was shown that automatic control ofUAV is possible using a single-antenna GPS receiveronly. Single-antenna GPS receiver is used widely as anavigation sensor for numerous applications includingunmanned aerial vehicles (UAVs). It provides positionand velocity measurements, from which pseudo-attitudescan also be synthesized for a fixed wing aircraft. Thissuggests the potential of single-antenna GPS receiver asthe sole sensor of the aircraft. Based on the experience ofprevious work, this paper develops the flight controlsystem for a small endurance UAV only using a low-costsingle-antenna GPS receiver that provides navigationsolution at 4 Hz. The small endurance UAV developed byKorea Aerospace Research Institute is a tailless flyingwingUAV with elevon and two wingtip rudders ascontrol surfaces. Linearized system models, which aredifferent from traditional fixed-wing aircraft, are obtainedby system identification process. Based on the identifiedmodel, linear quadratic regulator controllers are designed.Various simulations and flight tests are conducted toverify the developed system. During flight tests, inertialsensors such as gyros and accelerometers are not used atall to show the full potential of a single-antenna GPSreceiver based attitude determination system. Flight testresults verified again the value of proposed flight control system and showed that it could be applied to taillessflying-wing UAV successfully." @default.
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- W3119389933 date "2010-01-27" @default.
- W3119389933 modified "2023-09-27" @default.
- W3119389933 title "Design and Flight Test of Flight Control System for a Small Endurance UAV Only Using 4 Hz Single-Antenna GPS Receiver" @default.
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