Aerodynamic Design of Fixed-wing Mode for A Ducted-fan Tiltrotor UAV by Digital DATCOM-Reference-Cited by-同舟云学术

Aerodynamic Design of Fixed-wing Mode for A Ducted-fan Tiltrotor UAV by Digital DATCOM

Published:2022-06-21 Issue: Volume: Page:
ISSN:
Container-title:2022 International Conference on Unmanned Aircraft Systems (ICUAS)
language:
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Author:

Huang Jing¹,Wang Ban²,Deng Yangping²,Ning Kaikai¹,Zhang Youmin³

Affiliation:

1. Xi’an University of Technology,Department of Information and Control Engineering,Xi’an,Shaanxi,China,710048

2. Northwestern Polytechnical University,School of Aeronautics,Xi’an,Shaanxi,China,710072

3. Concordia University,Industrial and Aerospace Engineering,Department of Mechanical,Montreal,Quebec,Canada,H3G 1M8

Funder

National Natural Science Foundation of China

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/9836022/9835714/09836066.pdf?arnumber=9836066

Reference22 articles.

1. Verification challenges in F-16 ground collision avoidance and other automated maneuvers;heidlauf;ARCH18 5th International Workshop on Applied Verification of Continuous and Hybrid Systems,2018

2. Model-Based Design of a New Light-weight Aircraft

3. Aircraft coefficient comparisons between Datcom and published data;galbraith,2011

4. Estimation of nonlinear airship parameters using modular neural network

5. Exploitation of Thermals in Powered and Unpowered Flight of Autonomous Gliders

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Motion Equations and Attitude Control in the Vertical Flight of a VTOL Bi-Rotor UAV: Part 2;Electronics;2024-06-26

2. Nonlinear Modeling of Fixed-Wing Mode for a Ducted-Fan Tiltrotor UAV by DATCOM;Lecture Notes in Electrical Engineering;2023