Identification of a Non-Linear Landing Gear Model Using Nature-Inspired Optimization
This work deals with the application of a nature-inspired optimization technique to solve an inverse problem represented by the identification of an aircraft landing gear model. The model is described in terms of the landing gear geometry, internal volumes and areas, shock absorber travel, tire type...
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Main Authors: | , , , , |
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Format: | Article |
Language: | English |
Published: |
Wiley
2008-01-01
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Series: | Shock and Vibration |
Online Access: | http://dx.doi.org/10.1155/2008/246271 |
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