Active control of a non-linear landing gear system having...

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Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering 2017 / 06

Active control of a non-linear landing gear system having oleo pneumatic shock absorber using robust linear quadratic regulator approach

Yazici, Hakan, Sever, Mert
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Language:
english
Journal:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
DOI:
10.1177/0954410017713773
Date:
June, 2017
File:
PDF, 1009 KB
english, 2017
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