MANOEVRERINGSANORDNING FOR FLY

A maneuver force gradient system causes a helicopter, that otherwise tends to pitch up in a banked turn, to pitch nose-down. A command signal (25) is provided as a function of the roll angle to operate the longitudinal trim actuator (27) which automatically moves the cyclic control (50) resiliently...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	MURPHY, RICHARD DENNIS, CLELFORD, DOUGLAS HAROLD
Format:	Patent
Sprache:	nor
Schlagworte:	AEROPLANES AIRCRAFT AVIATION CONTROLLING COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS PHYSICS REGULATING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES TRANSPORTING
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