Patent · US Active

System and methods enabling aircraft energy dissipation for rapid decision making

US11790795B2 · kind B2 · utility

0Cited by
8References
20Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJun 2, 2020
Grant dateOct 17, 2023
Priority date
Expiry dateApr 29, 2041

Classification

  • Technology area (CPC G)Physics
  • CPC primaryG08G5/58
  • WIPO fieldControl
  • WIPO sectorInstruments

Abstract

A method in an aircraft for energy reduction is disclosed. The method includes: determining a starting point location, altitude and airspeed for a stable approach for landing at a diversion airport; and determining a vertical strategy for achieving the starting point altitude and airspeed by identifying a region of opportunity for adjusting the speed and altitude and identifying a plurality of energy reduction strategies for achieving the starting point altitude and airspeed while in the region of opportunity based on a speed mode during the stable approach. The method further comprises causing a graphic display to be displayed that lists for selection each of the plurality of identified strategies, detailed maneuver information for strategy implementation, and costs for implementing each identified strategy; and causing to be displayed, responsive to flight crew selection, a lateral view and vertical view of a proposed trajectory based on a selected identified strategy.

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