Method and apparatus for providing a dynamic thrust asymmetry rudder compensation command with no direct thrust measurement

A method and apparatus for producing a dynamic thrust asymmetry airplane rudder compensation command with no direct thrust measurement is disclosed. An excess thrust estimate based on measured acceleration along the flight path of the airplane and measured vertical speed of the airplane is low pass...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	LOCHTIE, DAVID W, DECK, TIMOTHY D
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIRCRAFT AVIATION CONTROLLING COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS PHYSICS REGULATING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES TRANSPORTING
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