Influence of Different Take-Off Weights on the Longitudinal Dynamic Stability of Flapping-Wing MAVs-Reference-Cited by-同舟云学术

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Influence of Different Take-Off Weights on the Longitudinal Dynamic Stability of Flapping-Wing MAVs

Published:2021-05 Issue:3 Volume:34 Page:04021006
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Xue Dong¹^ORCID,Song Bifeng²,Song Wenping²,Yang Wenqing³,Xu Wenfu⁴

Affiliation:

1. Associate Professor, School of Aeronautics, Northwestern Polytechnical Univ., Xi’an 710072, China (corresponding author). ORCID: .

2. Professor, School of Aeronautics, Northwestern Polytechnical Univ., Xi’an 710072, China.

3. Associate Professor, School of Aeronautics, Northwestern Polytechnical Univ., Xi’an 710072, China.

4. Professor, School of Mechanical Engineering and Automation, Harbin Institute of Technology, Shenzhen 518055, China.

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.1943-5525.0001241

Reference23 articles.

1. Influence of Center of Gravity Location on Flight Dynamic Stability in a Hovering Tailless FW-MAV: Longitudinal Motion

2. Effects of chordwise flexibility on the aerodynamic performance of a 3D flapping wing

3. Design, Aerodynamics, and Vision-Based Control of the DelFly

4. Keennon M. K. Klingebiel and H. Won. 2012. “Development of the Nano hummingbird: A tailless flapping wing micro air vehicle.” In Proc. 50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. Reston VA: American Institute of Aeronautics and Astronautics.

5. A multibody approach for 6-DOF flight dynamics and stability analysis of the hawkmoth Manduca sexta

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