Longitudinal and vertical gust feed forward compensation using lateral control surfaces

In one embodiment of a method to reduce vertical position errors of an aircraft, a disturbance input acting on the aircraft may be determined. The magnitude of the disturbance may be converted into a delta lift command if the magnitude of the disturbance is outside a criteria. The delta lift command...

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Bibliographische Detailangaben

Hauptverfasser:	Rupnik, Brian K, Flannigan, Sean J
Format:	Patent
Sprache:	eng
Online-Zugang:	Volltext bestellen
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