A commanded control signal is compared against an adaptive control signal in order to detect a rotor strike by a rotor included in an aircraft, wherein the adaptive control signal is associated with controlling the rotor and the adaptive control signal varies based at least in part on the commanded control signal and state information associated with the rotor. In response to detecting the rotor strike, a control signal to the rotor is adjusted in order to reduce a striking force associated with the rotor.
ROTOR STRIKE DETECTION AND FORCE REDUCTION
ROTORSCHLAGERKENNUNG UND KRAFTREDUZIERUNG
DÉTECTION DE FRAPPE DE ROTOR ET RÉDUCTION DE FORCE
2025-06-11
Patent
Electronic Resource
English
Online Contents | 1997
BIRD STRIKE SIMULATION FOR HELICOPTER ROTOR BLADES
British Library Conference Proceedings | 2013
|