2008-01-2263 Jam-Free, Fail-Safe Flight Control System with Asymmetric Load Alleviation Capability
Session, Aerodynamic design; structures, loads and vibrations; and stability and control, flying qualities and flight control system design ; 2008 ; Wichita, KS
Aerodynamic design; structures, loads and vibrations; and stability and control, flying qualities and flight control system design ; 2214 ; 69-72
SAE SP ; 2214
01.01.2008
4 pages
Held as part of the Wichita Aviation Technology congress and exhibition 2008. Includes bibliographical references.
Aufsatz (Konferenz)
Englisch
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