Modeling and Flight Control Simulation of a Quadrotor Tailsitter VTOL UAV
Author:
Affiliation:
1. Hong Kong University of Science and Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2017-1561
Reference20 articles.
1. A Hybrid Tricopter/Flying-Wing VTOL UAV
2. Design and wind tunnel tests of a tiltwing UAV
3. Quad Tilt Wing VTOL UAV: Aerodynamic Characteristics and Prototype Flight
4. Robust LPV H∞ gain-scheduled hover-to-cruise conversion for a tilt-wing rotorcraft in the presence of CG variations
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