Methods for testing multibeam satellite systems using input power telemetry and output noise power
View Patent ↗Methods that test multibeam satellite communication systems, including its antennas and transponders. The methods use input power telemetry and output noise power to test satellite transponders and antennas while the satellite is in orbit. One method that tests a satellite receive antenna employs at least two earth stations, one for RF testing and one for telemetry and commanding, with each providing a backup for the other. Other methods may use one or more earth stations to perform testing. Methods are disclosed that generate receive antenna pattern measurements, transmit pattern measurements, input chain frequency response curves, input chain transfer curves, and output chain frequency response curves.
1. A method of testing a satellite transmit antenna of a multibeam satellite system, comprising the steps of:
uplinking commands from an earth station to a satellite to cause a translation of the satellite;
transmitting downlink telemetry comprising orientation angles of the satellite from the satellite to a telemetry and command earth station;
measuring downlink noise in a small bandwidth at the telemetry and command earth station while the satellite is translated; and
processing the noise power level and orientation angles to verify operation of the transmit antenna on the satellite.
2. The method recited in claim 1 wherein the uplinked commands cause a slow constant attitude translation of the satellite.
3. The method recited in claim 1 wherein the uplinked commands cause a discrete steps in attitude translation of the satellite.
4. A method of generating an input chain frequency response curve for a multibeam satellite communication system, comprising the steps of:
positioning an uplink beam is over an earth station;
uplinking signals at different frequencies of interest from the earth station to the satellite;
generating downlink telemetry on-board the satellite that corresponds to the signal strengths of respective signals at the different frequencies;
transmitting the signal strength telemetry from the satellite to the earth station;
recording the signal strength telemetry and uplink frequency at the earth station; and
processing the recorded signal strength telemetry and uplink frequency to produce the input power frequency response curve.
5. The method recited in claim 4 wherein the signal strength telemetry is transmitted to a second earth station that is located at a geographically separate location from the uplinking earth station.
6. A method of generating an input chain transfer curve for a multibeam satellite communication system, comprising the steps of:
positioning an uplink beam is over an earth station;
uplinking RF signals at a plurality of power levels from the earth station to the satellite;
generating downlink telemetry on-board the satellite that corresponds to the signal strengths of respective signals at the different power levels;
transmitting the signal strength telemetry from the satellite to the earth station;
recording the signal strength telemetry at the earth station; and
processing the recorded signal strength telemetry to produce the input chain transfer curve corresponding to input power frequency response.
7. The method recited in claim 6 wherein the signal strength telemetry is transmitted to a second earth station that is located at a geographically separate location from the uplinking earth station.
8. A method of generating an output chain frequency response curve for a multibeam satellite communication system, comprising the steps of:
positioning a downlink beam is over an earth station;
measuring noise power of the downlink beam over a small bandwidth centered around a plurality of selected frequencies of interest at the earth station;
processing the noise power measurements to generate the output chain frequency response curve.
9. A method of generating a gain measurement of a transponder of a multibeam satellite communication system, comprising the steps of:
positioning a downlink beam is over an earth station;
measuring noise power of the downlink beam over a small bandwidth at a selected frequency at the earth station;
processing the recorded noise power measurements to generate a gain measurement of the transponder.
10. The method recited in claim 9 wherein the noise power of the downlink beam is measured at the center of the bandwidth at the selected frequency.