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 receive antenna of a multibeam satellite system, comprising the steps of:
uplinking a test signal from a payload test earth station to the receive antenna;
slewing the satellite over orientation angles using a slow constant attitude translation;
sensing a power level of the test signal on-board the satellite during slewing;
transmitting downlink telemetry comprising sensed power level and orientation angles of the satellite from the satellite to a telemetry and command earth station that is located at a geographically separate location from the payload test earth station; and
processing the sensed power level and said orientation angles to verify the operation of said receive antenna on the satellite.
2. The method recited in claim 1 wherein an edge of a satellite receive beam is chosen as a start point for slewing.
3. A method of testing a satellite receive antenna of a multibeam satellite system, comprising the steps of:
uplinking a test signal from a payload test earth station to the receive antenna;
slewing the satellite over orientation angles using a slow constant rate attitude translation;
sensing a power level of the test signal on-board the satellite during slewing;
transmitting downlink telemetry comprising sensed power level and orientation angles of the satellite from the satellite to a telemetry and command earth station that is located at a geographically separate location from the payload test earth station; and
processing the sensed power level and said orientation angles to verify the operation of said receive antenna on the satellite.
4. The method recited in claim 3 wherein an edge of a satellite receive beam is chosen as a start point for slewing.
5. A method of testing a satellite receive antenna of a multibeam satellite system, comprising the steps of:
uplinking a test signal from a first earth station to the receive antenna;
slewing the satellite over orientation angles using a slow constant rate attitude translation;
sensing a power level of the test signal on-board the satellite during slewing;
transmitting downlink telemetry comprising sensed power level and orientation angles of the satellite from the satellite to a second earth station that is located at a geographically separate location from the first earth station; and
processing the sensed power level and said orientation angles to verify the operation of said receive antenna on the satellite.
6. The method recited in claim 5 wherein an edge of a satellite receive beam is chosen as a start point for slewing.