Patent · US Expired

System for providing an integrated display of instantaneous information relative to aircraft attitude, heading, altitude, and horizontal situation

US4283705A · kind A · utility

41Cited by
4References
2Claims
0Family size

Inventors

Key dates

Filing dateMay 30, 1979
Grant dateAug 11, 1981
Priority date
Expiry dateMay 30, 1999

Classification

  • Technology area (CPC G)Physics
  • CPC primaryG01C23/00
  • WIPO fieldMeasurement
  • WIPO sectorInstruments

Abstract

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.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.