Modellunterstütze Geschwindigkeitsteuerung bei niedrigen Geschwindigkeiten für Drehflügelflugzeug

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: FOGLER, DONALD, L., JR., MILFORD, CT 06460, US, GOLD, PHILLIP, J., SHELTON, CT 06484, US, GLUSMAN, STEVEN, I., SPRINGFIELD, PA 19064, US, RICHARD, JAMES, L., STRATFORD, CT 06497, US
Format: Patent
Sprache:ger
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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).