Patent ID: 11952108
Assignee: SKYRYSE, INC.
Field: Transport (Mechanical engineering)
Classification: CPC B  G | IPC B

Claim 12:
13. A method performed by an avionics control router comprising a plurality of flight control computers of an aircraft, each flight control computer being part of a channel including a motor for an actuator corresponding to each of a plurality of aircraft components, the method comprising:
receiving, via a vehicle control interface of the aircraft, a flight control input;
generating, by the plurality of flight control computer of the avionics control router, actuator instructions for actuators in respective channels of the flight control computers based on the flight control input;
performing, by each flight control computer, a self-assessment;
performing, by each flight control computer, an assessment of other flight control computers of the avionics control router;
determining, using a voter in each channel, based on the self-assessment and the assessment of each flight control computer by the other flight control computers, a validity of the actuator instructions generated by each flight control computer; and
transmitting, in response to the actuator instructions being valid, the actuator instructions to the actuators.