Patent · US Active

System for guiding an aircraft to a reference point in low visibility conditions

US10096254B2 · kind B2 · utility

1Cited by
2References
25Claims
0Family size

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Key dates

Filing dateMar 3, 2011
Grant dateOct 9, 2018
Priority date
Expiry dateJun 1, 2031

Classification

  • Technology area (CPC G)Physics
  • CPC primaryG08G5/55
  • WIPO fieldControl
  • WIPO sectorInstruments

Abstract

A method of visually guiding a pilot flying an aircraft using one or more conformal symbols whose position is dynamically updated throughout the guidance is provided herein. The method includes the following stages: determining a desired flight route of an aircraft, based on a user-selected maneuver; presenting to a pilot, on a display, at least one 3D visual symbol that is: (i) earth-space stabilized, and (ii) positioned along a future location along the desired route; computing an updated desired route based on repeatedly updated aircraft flight data that include at least one of: location, speed, and spatial angle, of the aircraft; and repeating the presenting of the at least one 3D visual symbol with its updated location along the updated desired route.

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