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DLR institute Projects

hesham

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1973-1976
Dynamic wind tunnel simulation of a highly augmented flexible model aircraft with canard control surfaces. The test rig and model aircraft demonstrated open- and closed-loop control laws for variable stability functions, rigid body gust alleviation, and elastic mode suppression systems (Project BASE).

http://www.dlr.de/ft/desktopdefault.aspx/tabid-1388/1918_read-3396/
 

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hesham

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From Lotnictwo 5/2018.
 

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