Method and apparatus for correcting satellite imaging time
Disclosed is a method and apparatus for correcting a satellite image acquisition time. The method may include receiving, from a ground-based orbit propagator, an initially predicted imaging time, a correction command execution time, and a desired satellite position for imaging, and calculating a waiting time for imaging, a predicted satellite position, a correction time, and a corrected imaging time to correct a satellite image acquisition time.
1. A method of correcting a satellite image acquisition time to be implemented by a computer, the method comprising:
receiving, from a ground-based orbit propagator, a desired satellite position for imaging;
receiving, from a ground-based orbit propagator or a satellite-based orbit propagator, an initially predicted imaging time (T II ) and a correction command execution time (T Correct ),
calculating a waiting time for imaging;
obtaining a correction point-based satellite position from a satellite positioning system receiver, the correction point-based satellite position being a position of the satellite at the correction command execution time;
calculating a predicted satellite position using the correction point-based satellite position, the predicted satellite position being a position of the satellite at a time at which the waiting time elapses after the correction command execution time;
calculating a correction time; and
calculating a corrected imaging time.
2. The method of claim 1 , wherein the calculating of the waiting time comprises:
calculating the waiting time based on a difference between the initially predicted imaging time and the correction command execution time.
3. The method of claim 1 , wherein the calculating of the predicted satellite position comprises:
calculating the predicted satellite position using a satellite-based orbit propagator.
4. The method of claim 1 , wherein the calculating of the correction time comprises:
calculating the correction time by dividing a difference between the desired satellite position and the predicted satellite position by a satellite velocity.
5. The method of claim 1 , wherein the calculating of the correction time comprises:
calculating the correction time by dividing a difference between the desired satellite position and the correction point-based satellite position by a satellite velocity.
6. The method of claim 1 , wherein the calculating of the corrected imaging time comprises:
calculating the corrected imaging time by adding the correction time to the correction command execution time or the initially predicted imaging time.
7. The method of claim 1 , wherein the satellite positioning system receiver is configured to receive the correction point-based satellite position from one of a global positioning system (GPS), a global navigation satellite system (GLONASS), and a Galileo system.
8. An apparatus for correcting a satellite image acquisition time to be implemented by a computer, the apparatus comprising:
a processor configured to:
receive a desired satellite position for imaging from a ground-based orbit propagator,
receive an initially predicted imaging time and a correction command execution time from the ground-based orbit propagator or a satellite-based orbit propagator,
calculate a waiting time for imaging,
calculate a predicted satellite position using a correction point-based satellite position, the predicted satellite position being a position of the satellite at a time at which the waiting time elapses after the correction command execution time,
calculate a correction time, and
calculate a corrected imaging time; and
a satellite positioning system receiver configured to receive the correction point-based satellite position from a satellite positioning system, the correction point-based satellite position being a position of the satellite at the correction command execution time.
9. The apparatus of claim 8 , wherein the processor is further configured to calculate the waiting time based on a difference between the initially predicted imaging time and the correction command execution time.
10. The apparatus of claim 8 , wherein the processor is further configured to calculate the predicted satellite position using a satellite-based orbit propagator.
11. The apparatus of claim 8 , wherein the processor is further configured to calculate the correction time by dividing a difference between the desired satellite position and the predicted satellite position by a satellite velocity.
12. The apparatus of claim 8 , wherein the processor is further configured to calculate the correction time by dividing a difference between the desired satellite position and the correction point-based satellite position by a satellite velocity.
13. The apparatus of claim 8 , wherein the processor is further configured to calculate the corrected imaging time by adding the correction time to the correction command execution time or the initially predicted imaging time.
14. The apparatus of claim 8 , wherein the satellite positioning system is one of a global positioning system (GPS), a global navigation satellite system (GLONASS), and a Galileo system.
15. A non-transitory computer-readable storage medium storing instructions that, when executed by a processor, cause the processor to perform the method of claim 1 .