Patent · US Active

Variable energy management methods and systems

US11645924B2 · kind B2 · utility

0Cited by
8References
18Claims
0Family size

Assignee

Inventors

Key dates

Filing dateDec 18, 2020
Grant dateMay 9, 2023
Priority date
Expiry dateMay 26, 2041

Classification

  • Technology area (CPC G)Physics
  • CPC primaryG08G5/76
  • WIPO fieldControl
  • WIPO sectorInstruments

Abstract

Methods and systems are provided for assisting operation of a vehicle deviating from a desired manner of operation, such as an aircraft deviating from a planned trajectory. One method involves identifying a current aircraft altitude, identifying a current aircraft configuration, determining a recommended flight path from the current aircraft altitude for satisfying an upcoming constraint associated with a reference descent strategy based at least in part on the current aircraft configuration in response to a deviation between the current aircraft altitude a target altitude according to the reference descent strategy, and providing an output influenced by the recommended flight path. The recommended flight path includes a recommended vertical profile and a recommended speed profile, and the recommended flight path is configured to vary at least one of a kinetic energy or a potential energy of the aircraft along the recommended flight path en route to the upcoming constraint.

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