Load monitoring of aircraft landing gears using fiber optic sensors-Reference-Cited by-同舟云学术

Load monitoring of aircraft landing gears using fiber optic sensors

Published:2018-10 Issue: Volume:281 Page:31-41
ISSN:0924-4247
Container-title:Sensors and Actuators A: Physical
language:en
Short-container-title:Sensors and Actuators A: Physical

Author:

Iele A.,Leone M.,Consales M.,Persiano G.V.,Brindisi A.,Ameduri S.,Concilio A.,Ciminello M.,Apicella A.,Bocchetto F.,Cusano A.

Funder

Italian Ministry of University and Research

CAPRI - Carrello per Atterraggio con Attuazione Intelligente

Publisher

Elsevier BV

Subject

Electrical and Electronic Engineering,Metals and Alloys,Surfaces, Coatings and Films,Condensed Matter Physics,Instrumentation,Electronic, Optical and Magnetic Materials

Reference35 articles.

1. Aircraft Landing Gear Design and Development;Divakaran,2015

2. Aircraft Weight and Balance Handbook,2016

3. Analytical Investigation of Landing Dynamics of a Large Airplane With a Load-control System in the Main Landing Gear, NASA Technical Paper 1555;McGehee,1979

4. Aircraft Weight and Balance Handbook: FAA-H-8083-1A,2007

5. M. F. Almalki, M. Elshafei, Method and apparatus for tracking center of gravity of air vehicle, United States Patent Application Publication, US 2009/0143926 A1 (2009).

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