发明名称 AIRCRAFT VISION SYSTEM, AND ASSOCIATED VISION METHOD
摘要 The system according to the invention comprises a display and a synthetic image dynamic generating assembly. It includes a management assembly for the graphic interface of the display, capable of controlling the dynamic display, on a first region of the display, of a synthetic image and able to maintain, in certain movement configurations of the aircraft, a second region of the display delimited by the edge substantially with no synthetic surface representation of the terrain. The management assembly includes means for dynamically delimiting the edge of the first region. The delimiting means are configured to dynamically compute the position of the edge as a function of a determined visibility distance (DV), taken relative to the aircraft.
申请公布号 US2014214245(A1) 申请公布日期 2014.07.31
申请号 US201314043739 申请日期 2013.10.01
申请人 Dassault Aviation 发明人 BAUDSON Olivier;TURPIN Arnaud
分类号 B64D45/00 主分类号 B64D45/00
代理机构 代理人
主权项 1. A vision system for an aircraft, comprising: a display; an assembly for dynamically generating synthetic images, the synthetic images comprising at least one synthetic surface representation of the terrain situated facing the aircraft; a graphic interface management assembly for the display, capable of controlling the dynamic display, on a first region of the display, of a synthetic image coming from the synthetic image generating assembly, the first region being delimited by an edge, the management assembly being capable of maintaining, in certain movement configurations of the aircraft, a second region of the display delimited by the edge substantially with no synthetic surface representation of the terrain; characterized in that the management assembly includes means for dynamically delimiting the edge of the first region, the delimiting means being configured to compute the position of the edge of the first region on the display dynamically as a function of a determined visibility distance (DV), taken relative to the aircraft.
地址 Paris FR