LOW SPEED MODEL FOLLOWING VELOCITY COMMAND SYSTEM FOR ROTARY WING AIRCRAFT

A helicopter flight control system (21) includes a model following control system architecture which operates in a velocity command mode at low ground speeds. The control system processes information from a variety of helicopter sensors (31) in order to provide a command signal to the main rotor (11...

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Bibliographische Detailangaben
Hauptverfasser:	GLUSMAN, STEVEN L, RICHARD, JAMES L, GOLD, PHILLIP J, FOGLER, JR., DONALD L
Format:	Patent
Sprache:	eng
Schlagworte:	AEROPLANES AIRCRAFT AVIATION CHEMISTRY CONTROLLING COSMONAUTICS HELICOPTERS HETEROCYCLIC COMPOUNDS HUMAN NECESSITIES HYGIENE MEDICAL OR VETERINARY SCIENCE METALLURGY ORGANIC CHEMISTRY PERFORMING OPERATIONS PHYSICS PREPARATIONS FOR MEDICAL, DENTAL, OR TOILET PURPOSES REGULATING SPECIFIC THERAPEUTIC ACTIVITY OF CHEMICAL COMPOUNDS ORMEDICINAL PREPARATIONS SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES TRANSPORTING
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Beschreibung
Zusammenfassung:	A helicopter flight control system (21) includes a model following control system architecture which operates in a velocity command mode at low ground speeds. The control system processes information from a variety of helicopter sensors (31) in order to provide a command signal to the main rotor (11) of the helicopter which results in a ground speed which is proportional to the input provided via a sidearm controller (29).