Attitude and Altitude Stabilization of Fixed Wing VTOL Unmanned Air Vehicle
Author:
Affiliation:
1. ROKETSAN Missile Industries, Inc.
2. Middle East Technical University
3. Atilim University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-3378
Reference27 articles.
1. Modeling and control of a novel tilt — Roll rotor quadrotor UAV
2. Modelling, simulation and implementation of a quadrotor UAV
3. Trajectory-tracking control design for an under-actuated quadrotor
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