Patent · US Active

UAV hardware architecture

US11231726B2 · kind B2 · utility

1Cited by
6References
20Claims
0Family size

Assignee

Inventors

Key dates

Filing dateAug 28, 2018
Grant dateJan 25, 2022
Priority date
Expiry dateDec 5, 2038

Classification

  • Technology area (CPC G)Physics
  • CPC primaryG06T2207/30261
  • WIPO fieldAudio-visual technology
  • WIPO sectorElectrical engineering

Abstract

An unmanned aerial vehicle (UAV) includes one or more propulsion units that effect flight of the UAV, an application processing circuit configured to verify a validity of a system image of the UAV in a secure environment, and a flight control circuit operably coupled to the application processing circuit. Generation and/or transmission of control signals from the flight control circuit to one or more electronic speed controllers (ESC controllers) is prevented prior to verification of the validity of the system image.

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