Flight Control for Quadrotor Safety in the Presence of CoG Shift and Loss of Motor Efficiency-Reference-Cited by-同舟云学术

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Flight Control for Quadrotor Safety in the Presence of CoG Shift and Loss of Motor Efficiency

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

Jia Jindou¹,Guo Kexin²,Wang Chenliang¹,Shen Ning³,Jia Wei⁴,Yu Xiang¹

Affiliation:

1. Beihang University,School of Automation Science and Electrical Engineering,Beijing,China,100191

2. Beihang University,School of Aeronautic Science and Engineering,Beijing,China,100191

3. China North Industries Group Co,Xi’an Modern Control Technology Research Institute,Xi’an,China,710000

4. Xi’an ASN Technology Group Co., Ltd,Xi’an,China,710075

Funder

National Key Research and Development Program of China

National Natural Science Foundation of China

Technology Development

Research and Development

Natural Science Foundation of Zhejiang Province

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/9836022/9835714/09836202.pdf?arnumber=9836202

Reference29 articles.

1. Switching model predictive attitude control for a quadrotor helicopter subject to atmospheric disturbances

2. Attitude control for quadrotors subjected to wind disturbances via active disturbance rejection control and integral sliding mode control

3. Disturbance-Observer-Based Control and Related Methods—An Overview

4. An enhanced anti-disturbance attitude control law for flexible spacecrafts subject to multiple disturbances

5. Disturbance Observer Based Hovering Control of Quadrotor Tail-Sitter VTOL UAVs Using Synthesis

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