Patent · US Active

Methods and systems for fall back flight control configured for use in electric aircraft

US11724797B2 · kind B2 · utility

0Cited by
2References
20Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJul 1, 2021
Grant dateAug 15, 2023
Priority date
Expiry dateJul 25, 2041

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64D45/0005
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A system of fall back flight control configured for use in electric aircraft includes an input control configured to receive a pilot input and generate a control datum. System includes a flight controller communicatively coupled to the input control and configured to receive the control datum and generate an output datum. The system includes the actuator having a primary mode in which the actuator is configured to move the at least a portion of the electric aircraft as a function of the output datum and a fall back mode in which the actuator is configured to move the at least a portion of the aircraft as a function of the control datum. The actuator configured to receive the control datum, receive the output datum, detect a loss of communication with the flight controller, and select the fall back mode as a function of the detection.

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