Promoting both passenger comfort and aircraft handling of 6 DOF landing gear utilizing variable mechanical admittance approach-Reference-Cited by-同舟云学术

Promoting both passenger comfort and aircraft handling of 6 DOF landing gear utilizing variable mechanical admittance approach

Published:2020-04-02 Issue: Volume:30 Page:79-85
ISSN:2345-0533
Container-title:Vibroengineering PROCEDIA
language:
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Author:

Pirooz Mehran,Mirmahdi Seyed Hossein,Moafi Seyedeh Razieh

Publisher

JVE International Ltd.

Link

https://www.jvejournals.com/article/21221/pdf

Reference21 articles.

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2. An investigation of an active landing gear system to reduce aircraft vibrations caused by landing impacts and runway excitations;Wang;Journal of Sound and Vibration,2008

3. Adaptive landing gear: optimum control strategy and potential for improvement;Mikułowski;Shock and Vibration,2009

4. Mathematical model and vibration analysis of aircraft with active landing gear system using linear quadratic regulator technique;Toloei;International Journal of Engineering-Transactions B: Applications,2016

5. Landing gear suspension control through adaptive backstepping techniques with H∞ performance;Zapateiro;IFAC Proceedings Volumes,2011

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1. Semi-active control implementation in aircraft landing gear systems using hardware-in-the-loop test bench;Engineering Research Express;2024-08-06

2. Active Vibration Control of Landing Gear System;Düzce Üniversitesi Bilim ve Teknoloji Dergisi;2024-07-31

3. Linear Quadratic Gaussian Control of a 6-DOF Aircraft Landing Gear;Energies;2023-09-30

4. Linear and Nonlinear Models for Drop Simulation of an Aircraft Landing Gear System with MR Dampers;Actuators;2023-07-13

5. Robust force and displacement control of an active landing gear for vibration reduction at touchdown and during taxiing;SN Applied Sciences;2021-03-03