Course correction method and device, and aircraft
OwnerKang WANGinventor
Life of this patent
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Abstract
A method for correcting a course of an aircraft includes obtaining a flight velocity of the aircraft in a horizontal direction at a current time instance and acceleration data of the aircraft at the current time instance during a course movement of the aircraft. The method also includes correcting the acceleration data based on the flight velocity in the horizontal direction at the current time instance to obtain corrected acceleration data. The method further includes controlling a flight velocity of the aircraft in the horizontal direction based on the corrected acceleration data.
Claims20
A method for correcting a course of an aircraft, comprising:
- obtaining a flight velocity of the aircraft in a horizontal direction at a current time instance and acceleration data of the aircraft at the current time instance during a course movement of the aircraft;
- correcting the acceleration data based on the flight velocity in the horizontal direction at the current time instance to obtain corrected acceleration data;
- and
- controlling a flight velocity of the aircraft in the horizontal direction based on the corrected acceleration data.
A device for correcting a course of an aircraft, comprising:
- a velocity sensor;
- an accelerometer;
- and
- a processor,
- wherein the velocity sensor is configured to obtain a flight velocity of the aircraft in a horizontal direction at a current time instance and transmit the flight velocity to the processor during a course movement of the aircraft,
- wherein the accelerometer is configured to obtain acceleration data of the aircraft at the current time instance and transmit the acceleration data to the processor during the course movement of the aircraft, and
- wherein the processor is configured to:
- correct the acceleration data based on the flight velocity of the aircraft in the horizontal direction at the current time instance to obtain corrected acceleration data;
- and
- control a flight velocity of the aircraft in the horizontal direction based on the corrected acceleration data.
Dependencies are inferred from the claim text.