An embodiment rotorcraft (101) includes a main rotor, one or more flight controls connected to the main rotor and operational to control flight characteristics of the main rotor by pitching a nose of the rotorcraft (101) upward, and a flight control computer (FCC) (205) operable to determine an attitude command and to generate an adjusted attitude command by adjusting a magnitude of the attitude command according to an above ground level (AGL) altitude of the rotorcraft (101). The FCC (205) is further operable to control a flight characteristic of the rotorcraft (101) by sending the adjusted attitude command to one or more flight controls.
SYSTEM AND METHOD FOR AUTOMATIC ROTORCRAFT TAIL STRIKE PROTECTION
SYSTEM UND VERFAHREN FÜR AUTOMATISCHEN HECKSCHLAGSCHUTZ EINES DREHFLÜGELFLUGZEUGES
SYSTÈME ET PROCÉDÉ DE PROTECTION DE FRAPPE DE QUEUE DE GIRAVION AUTOMATIQUE
29.11.2023
Patent
Elektronische Ressource
Englisch
System and method for automatic rotorcraft tail strike protection
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