发明名称 System for providing an integrated display of instantaneous information relative to aircraft attitude, heading, altitude, and horizontal situation
摘要 A display device particularly suited for providing the pilot of an aircraft with combined inflight attitude, heading, altitude, and horizontal situation information previously available only by using two or three devices providing separate displays. The preferred embodiment of this invention combines a commonly used and commercially available flight director-type device for providing a display in combination with a miniature aircraft supported for angular displacement from a vertical orientation to indicate heading error, or heading offset, and an extended course deviation indicator bar which projects into juxtaposition with the miniature aircraft for providing a true picture of the aircraft's horizontal situation relative to a selected VOR, ILS, or MLS course.
申请公布号 US4283705(A) 申请公布日期 1981.08.11
申请号 US19790043942 申请日期 1979.05.30
申请人 JAMES, ROBERT;LOVELACE, ALAN M. 发明人 JAMES, ROBERT;LOVELACE, ALAN M.
分类号 G01C23/00;G01D7/04;(IPC1-7):G08G5/00 主分类号 G01C23/00
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