Modellunterstütze Geschwindigkeitsteuerung bei niedrigen Geschwindigkeiten für Drehflügelflugzeug.

摘要

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).