Patent · US Active

Flight control method and unmanned unmannered aerial vehicle

US10235893B2 · kind B2 · utility

1Cited by
1References
20Claims
0Family size

Assignee

Inventors

Key dates

Filing dateApr 5, 2017
Grant dateMar 19, 2019
Priority date
Expiry dateApr 5, 2037

Classification

  • Technology area (CPC G)Physics
  • CPC primaryG01S17/00
  • WIPO fieldControl
  • WIPO sectorInstruments

Abstract

A method for controlling an aerial vehicle includes determining a direction in which the aerial vehicle is traveling; determining, with reference to a table, an altitude range which corresponds to the determined direction and within which the aerial vehicle is caused to fly, the table indicating correspondences between directions in which the aerial vehicle is traveling and altitude ranges within which the aerial vehicle is to fly; obtaining, from an altimeter, a first altitude, which is a current altitude, at which the aerial vehicle is flying; determining whether the first altitude is included in the determined altitude range; and if it is determined that the first altitude is not included in the determined altitude range, changing an altitude at which the aerial vehicle is caused to fly from the first altitude to a second altitude included in the determined altitude range.

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