AIRCRAFT AND METHOD FOR DETERMINING LOADS ACTING ON AN AIRCRAFT

An aircraft comprises a control computer, an internal or external load determining unit, a first, central inertial measurement device and at least one additional second inertial measurement device, which is at a distance from the first inertial measurement device, wherein the load determining unit i...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	HICKETHIER, Holger, MEISNER, Christoph, STOLZ, Christian, VIDY, Cyrille
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	MEASURING PHYSICS TESTING TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR
Online-Zugang:	Volltext bestellen
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