Patent ID: 11964756
Assignee: AERHART, LLC
Field: Transport (Mechanical engineering)
Classification: CPC B  G | IPC B  G

Claim 11:
12. The aeronautical apparatus of claim 8, wherein;
the ECU determines actual trajectory of the aeronautical apparatus based on data from a sensor;
the ECU determines desired trajectory of the aeronautical apparatus based on at least one input signal;
the ECU commands the first, second, third, and fourth thrust-angle motors and the first, second, third, and fourth propeller motors are based on the actual trajectory and the desired trajectory; and
the sensor comprises at least one of: air speed, ground speed, radar altimeter, barometric pressure, thermometer, magnetometer, global position, accelerometer, gyroscope, radar, LIDAR, sonar, infrared camera, visible wavelength camera, energy consumption rate, energy generation rate, and battery charge state.