INTEGRATED HOVER DISPLAY WITH AUGMENTED APPROACH TO HOVER SYMBOLOGY CUEING FOR DEGRADED VISUAL ENVIRONMENTAL CONDITIONS

摘要

A flight control system 100 includes a primary flight display 118 having a hover display 114 which facilitates operations in DVE conditions. The hover display 114 includes a radar altitude display 122, heading drift symbology 134 and lateral drift symbology 142 which assists pilots in the detection of drift, which is common in DVE situations and to provide the pilot with a salient cue pertinent to the approach to hover and landing.