A novel constrained optimal tuning method with application to helicopter rotor track and balance-Reference-Cited by-同舟云学术

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A novel constrained optimal tuning method with application to helicopter rotor track and balance

Published:2023-02 Issue: Volume:184 Page:109715
ISSN:0888-3270
Container-title:Mechanical Systems and Signal Processing
language:en
Short-container-title:Mechanical Systems and Signal Processing

Author:

Wang Chuanda,Huang Guoke,Li Fei,Yu Guorui,Yi Hui,Peng Haijun

Funder

National Natural Science Foundation of China

Fundamental Research Funds for the Central Universities

Publisher

Elsevier BV

Subject

Computer Science Applications,Mechanical Engineering,Aerospace Engineering,Civil and Structural Engineering,Signal Processing,Control and Systems Engineering

Reference43 articles.

1. Pilot head and neck response to helicopter whole body vibration and head-supported mass;Law,2017

2. Analysis of autogyro rotor balancing and vibration;Vainilavičius,2015

3. A theory for bistable vibration isolators;Yan;Mech. Syst. Signal Proc.,2020

4. Cockroach-inspired structure for low-frequency vibration isolation;Ling;Mech. Syst. Signal Proc.,2022

5. Rotor track and balance improvements;Bechhoefer,2013

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