Control of Landing Efficiency of an Aircraft Landing Gear System With Magnetorheological Dampers-Reference-Cited by-同舟云学术

Control of Landing Efficiency of an Aircraft Landing Gear System With Magnetorheological Dampers

Published:2019-09 Issue:5 Volume:56 Page:1980-1986
ISSN:1533-3868
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Han Chulhee,Kang Byung-Hyuk,Choi Seung-Bok,Tak Jun Mo,Hwang Jai-Hyuk

Funder

Ministry of Trade, Industry and Energy

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference25 articles.

1. Aircraft Landing Gear Design: Principles and Practices

2. Aircraft Landing Gear Dynamics: Simulation and Control

3. HyunY. O. “Semi-Active Force Control of Landing Gear Using Magneto-Rheological Damper,” Ph.D. Thesis, Korea Aerospace Univ., Gyeong-gi, Republic of Korea, 2009.

4. Analysis and Control of a Magnetorheological Landing Gear System for a Helicopter

5. GA-Based Model Predictive Control of Semi-Active Landing Gear

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