System Parameter Identification for a Quadrotor UAV by Frequency Domain Method-Reference-Cited by-同舟云学术

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System Parameter Identification for a Quadrotor UAV by Frequency Domain Method

Published:2021-10-22 Issue: Volume: Page:
ISSN:
Container-title:2021 China Automation Congress (CAC)
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Author:

Huang Jing¹,Li Dong²,Wang Ban³,Zhang Youmin⁴,Mu Lingxia¹,Jiao Shangbin¹,Liu Han¹

Affiliation:

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

2. Jiujiang Precision Test Technology Research Institute,Jiujiang,China,332000

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

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

Funder

National Natural Science Foundation of China

Natural Science Foundation of Shaanxi Province

Natural Sciences and Engineering Research Council of Canada

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/9727224/9727236/09727528.pdf?arnumber=9727528

Reference15 articles.

1. System Identification and Flight Control of an Unmanned Quadrotor

2. System Identification Guidance for Multirotor Aircraft: Dynamic Scaling and Test Techniques

3. Identification of Low Order Equivalent Transfer Function Model of Trex-700E Helicopter from Flight Test Data

4. Time-Domain System Identification for Long-EZ Fixed-Wing Aircraft Based on Flight Test Data

5. Flight dynamic characteristics of canard rotor/wing aircraft in hover [J];gao;Chinese Journal of Aeronautics,2017

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. Cascaded Trajectory Tracking Control for A Quadcopter UAV with Consideration of Actuator Dynamics;2022 41st Chinese Control Conference (CCC);2022-07-25

2. Aerodynamic Design of Fixed-wing Mode for A Ducted-fan Tiltrotor UAV by Digital DATCOM;2022 International Conference on Unmanned Aircraft Systems (ICUAS);2022-06-21

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