System and method for aligning a multi-satellite receiver antenna
View Patent ↗A system and method for aligning an outdoor antenna reflector unit (ODU) with multiple satellites is disclosed. The method may rely on multiple satellites as alignment anchor points to reduce ODU alignment pointing error. The method may require at least three measurements of signal power at different angles for each satellite link to determine the ODU antenna pattern for each satellite link. A peak angle is then calculated for each satellite link based on the determined satellite link ODU antenna pattern. Once the satellite link peak angles are determined, the average peak angle can be calculated and used for aligning the ODU to the multiple satellites. The method may further reduce pointing error by using satellites transmitting within the K a frequency band as alignment anchor points. The method may simplify ODU alignment by merely requiring an installer to adjust an ODU alignment screw based on the calculated average peak angle.
1. A method comprising:
receiving signal power information for a multi-satellite outdoor antenna reflector unit (ODU);
based on the signal power information, determining, by a computing device, a first peak angle for the ODU to establish a first satellite link with a first satellite;
based on the signal power information, determining, by the computing device, a second peak angle for the ODU to establish a second satellite link with a second satellite;
determining an average peak angle based at least in part on the determined first peak angle and second peak angle; and
providing, on a graphical user interface, an indication of the average peak angle to facilitate alignment of the ODU to concurrently establish both the first and the second satellite links.
2. The method of claim 1 , wherein receiving the signal power information comprises:
for each of the first and the second satellite link, receiving at least three signal power measurements, wherein the three signal power measurements are determined at three different orientations of the ODU with respect to the corresponding one of the first and the second satellite.
3. The method of claim 1 , wherein the first satellite transmits signals within a frequency band of 18.3 Gigahertz to 20.2 Gigahertz.
4. The method of claim 1 , wherein providing the indication of the average peak angle on the graphical user interface comprises:
providing, on the graphical user interface, the average peak angle as a number of screw turns.
5. The method of claim 1 , wherein the first satellite link is characterized by a right hand circular polarization.
6. The method of claim 5 further comprising:
determining a third peak angle to establish a third satellite link with the first satellite, wherein the third satellite link is characterized by a left hand circular polarization;
wherein the determining of the average peak angle is further based on the third peak angle.
7. The method of claim 1 , wherein the average peak angle is for alignment of the ODU in elevation.
8. A non-transitory computer-readable medium storing instructions that are executable by one or more computing devices, wherein executing the instructions causes the one or more computing devices to perform functions comprising:
receiving signal power information for a multi-satellite outdoor antenna reflector unit (ODU);
based on the signal power information, determining a first peak angle for the ODU to establish a first satellite link with a first satellite;
based on the signal power information, determining a second peak angle for the ODU to establish a second satellite link with a second satellite;
determining an average peak angle based at least in part on the determined first peak angle and second peak angle; and
providing, on a graphical user interface, an indication of the average peak angle to facilitate alignment of the ODU to concurrently establish both the first and the second satellite links.
9. The non-transitory computer-readable medium of claim 8 , wherein receiving the signal power information comprises:
for each of the first and the second satellite link, receiving at least three signal power measurements, wherein the three signal power measurements are determined at three different orientations of the ODU with respect to the corresponding one of the first and the second satellite.
10. The non-transitory computer-readable medium of claim 8 , wherein the first satellite transmits signals within a frequency band of 26.18.35 Gigahertz to 20.2 Gigahertz.
11. The non-transitory computer-readable medium of claim 8 , wherein providing the indication of the average peak angle on the graphical user interface comprises:
providing, on the graphical user interface, the average peak angle as a number of screw turns.
12. The non-transitory computer-readable medium of claim 8 , wherein the first satellite link is characterized by a right hand circular polarization.
13. The non-transitory computer-readable medium of claim 12 , wherein the instructions cause the computing device to perform functions further comprising:
determining a third peak angle to establish a third satellite link with the first satellite, wherein the third satellite link is characterized by a left hand circular polarization;
wherein the determining of the average peak angle is further based on the third peak angle.
14. The non-transitory computer-readable medium of claim 8 , wherein the average peak angle is for alignment of the ODU in elevation.
15. A system comprising:
a multi-satellite outdoor antenna reflector unit (ODU);
a signal power measurement device that determines a signal power of a signal received by the ODU; and
a peak angle calculation device comprising:
a processor; and
a memory storing instructions that when executed by the processor cause the device to perform functions comprising:
receiving signal power information for the ODU;
based on the signal power information, determining a first peak angle for the ODU to establish a first satellite link with a first satellite;
based on the signal power information, determining a second peak angle for the ODU to establish a second satellite link with a second satellite;
determining an average peak angle based at least in part on the determined first peak angle and second peak angle; and
providing an indication of the average peak angle to facilitate alignment of the ODU to concurrently establish both the first and the second satellite links.
16. The system of claim 15 , wherein receiving the signal power information comprises:
for each of the first and the second satellite link, receiving at least three signal power measurements, wherein the three signal power measurements are determined at three different orientations of the ODU with respect to the corresponding one of the first and the second satellite.
17. The system of claim 15 , wherein the first satellite transmits signals within a frequency band of 18.3 Gigahertz to 20.2 Gigahertz.
18. The system of claim 15 , wherein providing the indication of the average peak angle comprises:
providing the average peak angle as a number of screw turns.
19. The system of claim 15 , wherein the first satellite link is characterized by a right hand circular polarization.
20. The system of claim 19 further comprising:
determining a third peak angle to establish a third satellite link with the first satellite, wherein the third satellite link is characterized by a left hand circular polarization;
wherein the determining of the average peak angle is further based on the third peak angle.