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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Hauptverfasser: GLUSMAN, STEVEN L, RICHARD, JAMES L, GOLD, PHILLIP J, FOGLER, JR., DONALD L
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creator GLUSMAN
STEVEN L
RICHARD
JAMES L
GOLD
PHILLIP J
FOGLER, JR.
DONALD L
description 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).
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subjects 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
title LOW SPEED MODEL FOLLOWING VELOCITY COMMAND SYSTEM FOR ROTARY WING AIRCRAFT
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