Research on helicopter electric tail rotor control method based on fuzzy neural network
Author:
Affiliation:
1. Aerospace University,Liaoning General Aviation Research Institute Shenyang,Shenyang,China
2. Shenyang Aerospace University,School of Artificial Intelligence,Shenyang,China
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx8/10587298/10587321/10588087.pdf?arnumber=10588087
Reference27 articles.
1. Aerodynamic Noise Characterization of Distributed Culvert Tail Rotor;Wang;Joumal of Nan**g University of Aeronautics & Astronautics/Nan**g Hangkong Hangtian Daxue Xuebao,2023
2. Analysis of strong magnetic environment interference of inspection rotary wing UAV
3. Conceptual design of a distributed electric anti-torque system for enhanced helicopter safety and performance
4. Development and Prospects of Helicopter Technology;Deng;*Aviation Science and Technology*,2021
5. Integration of CNN in a Dynamic Model-Based Controller for Control of a 2DOF Helicopter With Tail Rotor Perturbations
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