GUST COMPENSATION SYSTEM AND METHOD FOR AIRCRAFT

A gust compensation system 200 is configured to adaptively reduce gust loads exerted into an aircraft 100/500. The gust compensation system may include a first sensor 110 proximate to a front of the aircraft 100. The first sensor 110 is configured to output a first signal. A second sensor 120 may be...

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Bibliographische Detailangaben
Hauptverfasser: CAICEDO, Rafael E, STREFLING, Paul C, HO, Alexander C, SIU, Tze L, YAMASHIRO, Hisako, ABDEL-MOTAGALY, Khaled, KIOUMARS, Najmabadi, DALLARA, Christopher D
Format: Patent
Sprache:eng ; fre ; ger
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Zusammenfassung:A gust compensation system 200 is configured to adaptively reduce gust loads exerted into an aircraft 100/500. The gust compensation system may include a first sensor 110 proximate to a front of the aircraft 100. The first sensor 110 is configured to output a first signal. A second sensor 120 may be distally located from the front of the aircraft 100. The second sensor 120 is configured to output a second signal. A gust signal sub-system 202 is configured to receive the first and second signals and generate a gust signal 226 based on analysis of the first and second signals. The gust signal sub-system 202 outputs the gust signal 226 and may modify a load parameter signal 220 in response to the gust signal 226 exceeding a load alleviation threshold.