IDENTIFYING PILOT-INDUCED OSCILLATION TENDENCIES IN ADVANCED FLY-BY-WIRE ROTORCRAFT
IDENTIFYING PILOT-INDUCED OSCILLATION TENDENCIES IN ADVANCED FLY-BY-WIRE ROTORCRAFT
Four rail front crush structure with load dissemination into eight element support structure
FOUR RAIL FRONT CRUSH STRUCTURE WITH LOAD DISSEMINATION INTO EIGHT ELEMENT SUPPORT STRUCTURE