Patent ID: 11958591
Assignee: THE BOEING COMPANY
Field: Transport (Mechanical engineering)
Classification: CPC B | IPC B

Claim 6:
7. A system comprising:
a first actuator;
a second actuator;
a first output shaft;
a second output shaft;
a first cam;
a second cam;
a first drive arm coupled to the first output shaft and a control surface of an air vehicle;
a second drive arm coupled to the second output shaft and the control surface;
memory;
machine-readable instructions; and
processor circuitry to execute the machine-readable instructions to:
control the first actuator to cause the first actuator to operatively couple with the control surface via engagement between the first cam and the first output shaft; and
control the second actuator to cause the second actuator to operatively couple with the control surface via engagement between the second cam and the second output shaft.