Gust compensation system and method for aircraft

A gust compensation system is disclosed and configured to adaptively reduce gust loads exerted into an aircraft. The gust compensation system may include a first sensor proximate to a front of the aircraft. The first sensor is configured to output a first signal. A second sensor may be distally loca...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	CAICEDO RAFAEL E, YAMASHIRO HISAKO, ABDEL-MOTAGALY KHALED, HO ALEXANDER C, STREFLING PAUL C, NAJMABADI KLOUMARS, SIU TZE L, DALLARA CHRISTOPHER D
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AEROPLANES AIRCRAFT AVIATION CONTROLLING COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS PHYSICS REGULATING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES TRANSPORTING
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