The disclosure relates to a flight control system for a rotary aircraft, the rotary aircraft having a longitudinal controller, a lateral controller, a directional controller, and a vertical controller, the control system comprising a longitudinal loop design, a lateral loop design, a directional loop design and a vertical control loop design, a forward speed hold loop and a lateral speed hold loop automatically engaging when the longitudinal controller is returned to a detent position and the aircraft groundspeed is outside a first groundspeed threshold, longitudinal and lateral maneuverability being controlled by either a pitch attitude and lateral speed loop or a pitch rate and roll rate loop when the longitudinal controller is out of the detent position.
FLIGHT CONTROL LAWS FOR AUTOMATIC HOVER HOLD
FLUGSTEUERUNGSFUNKTIONEN ZUR AUTOMATISCHEN SCHWEBEFLUGSTEUERUNG
LOIS DE COMMANDES DE VOL POUR MAINTIEN AUTOMATIQUE EN VOL STATIONNAIRE
2016-09-07
Patent
Electronic Resource
English
Development of Modern Control Laws for the AH-64D in Hover/Low Speed Flight
British Library Conference Proceedings | 2006
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