Improved design of an active landing gear for a passenger aircraft using multi-objective optimization technique-Reference-Cited by-同舟云学术

Improved design of an active landing gear for a passenger aircraft using multi-objective optimization technique

Published:2018-12-12 Issue:5 Volume:59 Page:1813-1833
ISSN:1615-147X
Container-title:Structural and Multidisciplinary Optimization
language:en
Short-container-title:Struct Multidisc Optim

Author:

Zarchi Milad^ORCID,Attaran Behrooz

Publisher

Springer Science and Business Media LLC

Subject

Control and Optimization,Computer Graphics and Computer-Aided Design,Computer Science Applications,Control and Systems Engineering,Software

Link

http://link.springer.com/content/pdf/10.1007/s00158-018-2135-8.pdf

Reference47 articles.

1. Bender EK, Beiber M (1971) A feasibility study of active landing gear. AFFDL Technical Report 1:70–126

2. Bissell CC, Chapman DA (1992) Digital signal transmission (2nd ed.). Cambridge University Press, p 64 ISBN 978-0-521-42557-5

3. Catt T, Cowling D, and Shepard A. 1993. Active Landing Gear Control for Improved Ride Quality During Ground Roll. AGARD Smart Structures for Aircraft and Spacecraft, Conference Proceedings 531, Stirling Dynamics Ltd, Bristol

4. Christofer K (2013) Dynamic response analysis of generic nose landing gear as two dof system. In: International journal of scientific and engineering research

5. Currey NS (1998) Aircraft landing gear design: principles and practices. AIAA Education Series, Washington

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