Patent · US Active

Method and system for fly-by-wire flight control configured for use in electric aircraft

US11225321B1 · kind B1 · utility

5Cited by
6References
20Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMar 31, 2021
Grant dateJan 18, 2022
Priority date
Expiry dateMar 31, 2041

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T50/40
  • WIPO fieldComputer technology
  • WIPO sectorElectrical engineering

Abstract

In an aspect a system for fly-by-wire flight control configured for use in electric aircraft including at least a sensor, wherein the sensor is communicatively connected a pilot control and configured to detect a pilot input from the pilot control and generate, as a function of the pilot input, command datum. A system includes a flight controller, the flight controller including a computing device and configured to perform a voting algorithm, wherein performing the voting algorithm includes determining that the sensor is an allowed sensor, wherein determining that the sensor is an allowed sensor includes determining that the command datum is an active datum, determining the command datum is an admissible datum, generating, as a function of the command datum and the allowed sensor, a control surface datum wherein the control surface datum is correlated to the pilot input.

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