Shock and Vibration

Shock and Vibration / 2009 / Article

Open Access

Volume 16 |Article ID 732803 | https://doi.org/10.3233/SAV-2009-0460

Grzegorz Mikułowski, Łukasz Jankowski, "Adaptive Landing Gear: Optimum Control Strategy and Potential for Improvement", Shock and Vibration, vol. 16, Article ID 732803, 20 pages, 2009. https://doi.org/10.3233/SAV-2009-0460

Adaptive Landing Gear: Optimum Control Strategy and Potential for Improvement

Received17 Jul 2007
Revised07 Mar 2008

Abstract

An adaptive landing gear is a landing gear (LG) capable of active adaptation to particular landing conditions by means of controlled hydraulic force. The objective of the adaptive control is to mitigate the peak force transferred to the aircraft structure during touch-down, and thus to limit the structural fatigue factor. This paper investigates the ultimate limits for improvement due to various strategies of active control. Five strategies are proposed and investigated numerically using a~validated model of a real, passive landing gear as a reference. Potential for improvement is estimated statistically in terms of the mean and median (significant) peak strut forces as well as in terms of the extended safe sinking velocity range. Three control strategies are verified experimentally using a laboratory test stand.

Copyright © 2009 Hindawi Publishing Corporation. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.


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