Systems and Methods for Pitch Axis Envelope Limiting of an Aircraft

The invention relates to systems and methods for pitch axis envelope limiting of an aircraft. An example method of limiting an aircraft to a pitch axis envelope includes determining aircraft state limits associated with multiple pitch axis variables of an aircraft, determining predicted aircraft sta...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	MILLS NIKOS D, FLANZER TRISTAN C, LY UY-LOI, NAJMABADI KIOUMARS, HAUGEBERG HEIDI M
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
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