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

摘要

A flight control system includes a primary flight display having a hover display which facilitates operations in DVE conditions. The hover display includes a radar altitude display, heading drift symbology and lateral drift symbology 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.