Numerical Study of Aerodynamic Performance of a Multirotor Unmanned-Aerial-Vehicle Configuration
Author:
Affiliation:
1. Department of Aerospace Engineering, Korea Advanced Institute of Science and Technology, Daejeon 305-701, Republic of Korea
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C032828
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1. Quadrotor Helicopter Flight Dynamics and Control: Theory and Experiment
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