SYSTEM AND METHOD FOR CONTROLLING FUEL FLOW TO A GAS TURBINE ENGINE BASED ON MOTION SENSOR DATA

A system for an aircraft having a first gas turbine engine and a second gas turbine engine includes a first engine controller comprising a first motion sensor. The first motion sensor defines a firstorthogonal coordinate system, and is configured for determining first motion sensor data indicating motion of the aircraft along at least one axis of the first orthogonal coordinate system. The systemfurther includes a second engine controller comprising a second motion sensor spaced apart from the first motion sensor. The second motion sensor defines a second orthogonal coordinate system, and isconfigured for determining second motion sensor data indicating motion of the aircraft along at least one axis of the second orthogonal coordinate system. In addition, the second engine controller iscommunicatively coupled to the first engine controller such that the first engine controller receives the second motion sensor data. 一种用于具有第一燃气涡轮发动机和第二燃气涡轮发动机的飞行器的系统，该系统包含第一发动机控制器，其包括第一运动传感器。第一运动传感器限定第一正交坐标系，并且被构造为用于确定第一运动传感器数据