Improved Aerodynamic Analysis for Multirotor-Type UAS Flight Simulation Using Dynamic Inflow and Rigid Blade Flapping-Reference-Cited by-同舟云学术

Improved Aerodynamic Analysis for Multirotor-Type UAS Flight Simulation Using Dynamic Inflow and Rigid Blade Flapping

Published:2020-07 Issue:4 Volume:33 Page:04020021
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Park SunHoo¹,Yoo JeongUk¹,Shin SangJoon²

Affiliation:

1. Graduate Student, Dept. of Mechanical and Aerospace Engineering, Seoul National Univ., 1 Gwanak-ro, Gwanak-gu, Seoul 08826, Republic of Korea.

2. Professor, Dept. of Mechanical and Aerospace Engineering, Seoul National Univ., 1 Gwanak-ro, Gwanak-gu, Seoul 08826, Republic of Korea; Institute of Advanced Aerospace Technology, Seoul National Univ., 1 Gwanak-ro, Gwanak-gu, Seoul 08826, Republic of Korea (corresponding author).

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001135

Reference29 articles.

1. Bai Y. H. Liu Z. Shi and Y. Zhong. 2012. “Robust control of quadrotor unmanned air vehicles.” In Proc. 31st Chinese Control Conf. New York: IEEE.

2. Barcelos D. F. A. Kolaei and G. Bramesfeld. 2018. “Performance prediction of multirotor vehicles using a higher order potential flow method.” In Proc. 2018 AIAA Aerospace Sciences Meeting. Kissimmee FL: American Institute of Aeronautics and Astronautics.

3. Brandt B. J. and S. M. Selig. 2011. “Propeller performance data at low Reynolds numbers.” In Proc. 49th AIAA Aerospace Sciences Meeting. Orlando FL: American Institute of Aeronautics and Astronautics.

4. Bresciani T. 2008. “Modelling identification and control of a quadrotor helicopter.” M.S. thesis Dept. of Automatic Control Lund Univ. Lund Sweden.

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