Patent · US Active

Nonlinear fly-by-wire aircraft control

US12043370B2 · kind B2 · utility

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0References
20Claims
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Assignee

Inventors

Key dates

Filing dateAug 10, 2022
Grant dateJul 23, 2024
Priority date
Expiry dateOct 7, 2042

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64C2027/8209
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

There is disclosed in one example a flight control computer for a rotary aircraft, including: a first interface to communicatively couple to a flight control input; a second interface to communicatively couple to flight geometry actuators; a data source; a multi-dimensional lookup table including a data structure to correlate flight control inputs to flight geometry actuator outputs according to a third-factor; and circuitry and logic instructions to: receive an input via the first interface; query the data source for the third-factor; query the multi-dimensional lookup table for a control input modifier according to the flight control input and the third-factor; and compute and send via a third interface a flight geometry output according to the control input modifier.

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