Patent · US Active

Electrical vertical take-off and landing aircraft having reversionary flight control and method of use

US11353890B1 · kind B1 · utility

10Cited by
14References
20Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJun 16, 2021
Grant dateJun 7, 2022
Priority date
Expiry dateJun 16, 2041

Classification

  • Technology area (CPC G)Physics
  • CPC primaryG05D1/102
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

Aspects relate to methods and systems for reversionary flight control for an electrical vertical take-off and landing (eVTOL) aircraft. An exemplary system includes a pilot control, a sensor configured to sense and transmit analog control data associated with a pilot interaction with the pilot control, a pilot interface module configured to receive the analog control data, convert the analog control data to digital control data, and transmit digital control, an actuator, and a flight controller. The flight controller may be configured to receive the digital control data, determine a primary command datum as a function of the digital control data, transmit the primary command datum to the actuator, determine that the digital control signal is non-functional, receive the analog control data, determine a reversionary command datum as a function of the analog control data, and transmit the reversionary command datum to the actuator.

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