Study on adaptive torsional vibration suppression methods for helicopter/turboshaft engine system with variable rotor speed-Reference-Cited by-同舟云学术

Study on adaptive torsional vibration suppression methods for helicopter/turboshaft engine system with variable rotor speed

Published:2020-05-12 Issue: Volume: Page:
ISSN:1561-8625
Container-title:Asian Journal of Control
language:en
Short-container-title:Asian J Control

Author:

Wang Yong¹^ORCID,Zheng Qiangang^ORCID,Fu Dawei,Zhang Haibo

Affiliation:

1. College of Energy and Power EngineeringNanjing University of Aeronautics and Astronautics Nanjing China

Funder

National Natural Science Foundation of China

Publisher

Wiley

Subject

Control and Systems Engineering

Link

https://onlinelibrary.wiley.com/doi/pdf/10.1002/asjc.2294

Reference21 articles.

1. Possibilities and difficulties for rotorcraft using variable transmission drive trains;Amri H.;CEAS Aeronautical Journal,2016

2. G. E.Welch A. B.McVetta andM. A.Stevens et al.Variable‐speed power‐turbine research at Glenn Research Center. NASA/TM‐2012–217605 2012.

3. Disturbance Rejection Control for a Vibrating String System

4. H. A.DeSmidtet al. Comprehensive Modeling and Analysis of Rotorcraft Variable Speed Propulsion System With Coupled Engine/Transmission/Rotor Dynamics. NASA/CR‐2013‐216502.

5. D. V.Kalinin.MULTITHREADED CONTINUOUSLY VARIABLE TRANSMISSION SYNTHESIS FOR NEXT‐GENERATION HELICOPTERS. 29th Congress of International Council of the Aeronautical Science St. Petersburg Russia 2014.

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