ADAPTATION OF SELECTIVE FIELD ALERTS, BASED ON THE INSTANTANEOUS MANOEUVRABILITY OF A GIRAVION

摘要

The invention relates to the development of alerts for terrain avoidance by a rotary car aircraft (1), which provides for the development of an avoidance trajectory (TA) with a proximal section and a curve of avoidance (EC). The proximal section (25) is determined according to a wayheet of the aircraft (1), and the avoidance curve (CE) forms a distal section (24) having a conical curve and calculated according to the instantaneous maneuverability of the aircraft (1).