Parametric Investigation of the Flight Performance of a Variable Rotor Pitch X-Configuration Quadrotor Aircraft-Reference-Cited by-同舟云学术

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Parametric Investigation of the Flight Performance of a Variable Rotor Pitch X-Configuration Quadrotor Aircraft

Published:2022-11 Issue:6 Volume:35 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Han Dong¹,Zhou Linzhen²,Barakos George N.³

Affiliation:

1. Professor, College of Aerospace Engineering, Nanjing Univ. of Aeronautics and Astronautics, Nanjing 210016, China (corresponding author).

2. Research Assistant, College of Aerospace Engineering, Nanjing Univ. of Aeronautics and Astronautics, Nanjing 210016, China.

3. Professor, Computational Fluid Dynamics Laboratory, School of Engineering, Univ. of Glasgow, Glasgow G12 8QQ, Scotland, UK.

Publisher

American Society of Civil Engineers (ASCE)

Subject

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

Link

https://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001481

Reference20 articles.

1. Real-Time Closed-Loop System Identification of a Quadcopter

2. Energy based 3D trajectory tracking control of quadrotors with model-free based on-line disturbance compensation

3. Aerodynamic Interference Model for Multirotors in Forward Flight

4. Performance improvement of variable speed rotors by Gurney flaps

5. Numerical Study of Aerodynamic Performance of a Multirotor Unmanned-Aerial-Vehicle Configuration

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