Patent ID: 8892295

Claim:
A control and monitoring system comprising: sensors configured to sense status of a turbojet thrust reverser; a control and monitoring computing computer; a control unit configured to control the thrust reverser, the control unit being controlled by the control and monitoring computing computer as a function of information from the sensors supplied to the control and monitoring computing computer via the control unit; and a turbojet regulating device, the turbojet regulating device being controlled by the control and monitoring computing computer as a function of information from the sensors supplied to the control and monitoring computing computer via the control unit, wherein the control and monitoring computing computer and the control unit are electrically directly connected, the sensors are electrically directly connected to the control unit and the turbojet regulating device, the turbojet regulating device is electrically directly connected to the control and monitoring computing computer, and the control unit and the turbojet regulating device are not electrically connected together.