Design of Unmanned Helicopter Distributed Electric Tail Rotor Controller Based on Improved Active Disturbance Rejection Control-Reference-Cited by-同舟云学术

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Design of Unmanned Helicopter Distributed Electric Tail Rotor Controller Based on Improved Active Disturbance Rejection Control

Published:2024 Issue: Volume:12 Page:97053-97066
ISSN:2169-3536
Container-title:IEEE Access
language:
Short-container-title:IEEE Access

Author:

Zhang Qing-Xin¹^ORCID,Ji Yun-Feng²^ORCID,Wang Feng³,Pei Lei²,Cha Zheng-Ming⁴

Affiliation:

1. Key Laboratory of General Aviation, Shenyang Aerospace University, Shenyang, China

2. School of Artificial Intelligence, Shenyang Aerospace University, Shenyang, China

3. Liaoning General Aviation Academy, Shenyang, China

4. AVIC Changhe Aircraft Industry (Group) Corporation Ltd., Jingdezhen, China

Publisher

Institute of Electrical and Electronics Engineers (IEEE)

Link

http://xplorestaging.ieee.org/ielx8/6287639/10380310/10596295.pdf?arnumber=10596295

Reference34 articles.

1. Comprehensive evaluation technique research on the conceptual scheme of distributed electric drive anti-torque system for light helicopters;Tang;Aeronaut. Sci. Technol.,2023

2. Helicopter electric tail rotor technology development and prospects;Jian;Helicopter Technique,2021

3. Design robust H_∞ -PID controller for a helicopter system using sequential quadratic programming algorithm

4. An improved teaching-learning-based optimization algorithm with memetic method for global optimization;Tang;Int. J. Advancements Comput. Technol.,2013

5. Robust Control of 2-DoF Helicopter System in Presence of Unmatched Disturbances & Actuator Faults

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