Lead-Lag Damper Robustness Analysis for Helicopter Ground Resonance-Reference-Cited by-同舟云学术

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Lead-Lag Damper Robustness Analysis for Helicopter Ground Resonance

Published:2013-07 Issue:4 Volume:36 Page:1150-1161
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Quaranta Giuseppe¹,Muscarello Vincenzo¹,Masarati Pierangelo¹

Affiliation:

1. Dipartimento di Ingegneria Aerospaziale, Politecnico di Milano, 20156 Milan, Italy

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.57188

Reference25 articles.

1. Ground Vibrations of Helicopters

2. Robust Aeroservoelastic Stability Analysis

Cited by 13 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Impact of Design and Operational Parameters on Helicopter Vertical Bounce;J AM HELICOPTER SOC;2023

2. Stability Analysis of Nonlinear Rotating Systems Using Lyapunov Characteristic Exponents Estimated From Multibody Dynamics;Journal of Computational and Nonlinear Dynamics;2023-05-04

3. Damper model identification using mixed physical and machine-learning-based approach;The Aeronautical Journal;2023-03-03

4. A strategy to suppress limit cycle oscillations in helicopter ground resonance including landing gear nonlinearities;Aerospace Science and Technology;2020-10

5. An Analytical Method for Coaxial Helicopter Ground Resonance;MATEC Web of Conferences;2020

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