Satellite performance monitoring

• US 8,576,118 B2
• Filed: 01/28/2009
• Issued: 11/05/2013
• Est. Priority Date: 01/29/2008
• Status: Active Grant

• Current Assignee: ViaSat Incorporated
• Original Assignee: ViaSat Incorporated
• Inventors: Miller, Mark J.
• Primary Examiner(s): Pan, Yuwen
• Assistant Examiner(s): Wang, Fanghwa
• Application Number:
  US12/361,403
• Publication Number:
  US 20090195444A1
• Time in Patent Office: 1,742 Days
• Field of Search: None
• US Class Current: 342/352
• CPC Class Codes: H04B 17/40 of relay systems
• CPC Class Codes: H04B 7/185 Space-based or airborne stations; Stations for satellite systemsH04B7/204 takes precedence
• CPC Class Codes: H04B 7/18513 Transmission in a satellite or space-based system
• CPC Class Codes: Y02D 30/70 in wireless communication networks

Abstract

Techniques for monitoring transmission performance of a satellite communications systems are provided, including techniques for measuring the primary contributors to the end-to-end SNR, including the uplink SNR, the downlink SNR, and the C/I for each link in the network. These individual measurements are used to estimate satellite effective isotropic radiated power (EIRP), satellite antenna gain-to-noise-temperature (G/T), and loss due to an Earth Terminal pointing error. The EIRP, satellite antenna G/T and loss due to Earth terminal pointing error may then be used to determine operating parameters for the satellite communications network that enable the network to operate more efficiently.

Claims

1. A method used on a satellite communication system, wherein the satellite communications system includes a satellite, at least one gateway terminal and a plurality of user terminals, the method comprising:

measuring, at the at least one gateway terminal, a total receive power of a signal received from the satellite under normal operating conditions;

measuring one of a signal-only power and a signal-to-noise-plus-interference ratio (S1NR) for a signal received from the satellite under normal operating conditions;

measuring a total thermal noise component of the signal received from the satellite during a first quiet interval where uplink transmission from the at least one gateway and the plurality of user terminals have been disabled;

measuring a first out-of-band downlink thermal noise component and a first in-band downlink thermal noise component while the satellite is in a transmission disabled state;

determining a compensation factor using the first in-band downlink thermal noise component and the first out-of-band downlink thermal noise component;

measuring a second out-of-band downlink thermal noise component while the satellite is under normal operating conditions;

estimating a second in-band downlink thermal noise component of the signal received from the satellite by multiplying the second out-of-band downlink thermal noise component by the compensation factor; and

calculating satellite communication system operating parameters during satellite operation using the total receive power, the signal-only power or the SINR, measurements of the total thermal noise component, and the second in-band downlink thermal noise component for monitoring the performance of the satellite communication system in which the satellite is operating.

2. The method of claim 1 further comprising:

commanding the at least one gateway terminal and the plurality of user terminals to disable all transmissions prior to measuring the total thermal noise component of the signal received from the satellite; and

commanding the at least one gateway terminal and the plurality of user terminals to enable transmissions after measuring the total thermal noise component of the signal received from the satellite.

3. The method of claim 2 wherein an outage time used for measuring the total thermal noise component of the signal received from the satellite is built into a frame structure of the satellite communications system so that the outage time occurs at a regular interval.

4. The method of claim 2, further comprising:

scheduling an outage time for measuring the total thermal noise component of the signal received from the satellite, wherein the outage time is scheduled by a central control agent of the satellite broadcast system.

5. The method of claim 4 wherein scheduling an outage time for measuring the total thermal noise component of the signal received from the satellite further comprises:

commanding the at least one gateway terminal and the plurality of user terminals to disable all transmissions for an interval specified in a message.

6. The method of claim 2 wherein commanding the at least one gateway terminal to disable all transmissions prior to measuring the total thermal noise component of the signal received from the satellite further comprises:

calculating a path delay to the satellite from the at least one gateway terminal based on the location of the at least one gateway terminal and ephemeris data of the satellite; and

synchronously disabling the at least one gateway terminal with the disabling of the plurality of the user terminals using the path delay and an accurate time base of the at least one gateway terminal.

7. The method of claim 1, further comprising:

commanding the satellite to disable all transmissions prior to measuring the first in-band downlink thermal noise component and the first out-of-band downlink thermal noise component; and

commanding the satellite to enable transmissions after measuring the first in-band downlink thermal noise component and the first out-of-band downlink thermal noise component.

8. The method of claim 1 further comprising:

commanding the satellite, the at least one gateway terminal, and the plurality of user terminals to disable all transmissions prior to measuring the first in-band downlink thermal noise component and the first out-of-band downlink thermal noise component; and

commanding the satellite, the at least one gateway terminal, and the plurality of user terminals to enable transmissions after measuring the first in-band downlink thermal noise component and the first out-of-band downlink thermal noise component.

9. The method of claim 1 wherein both the signal only power of the signal received from the satellite under normal operating conditions and the SINR for the signal received from the satellite under normal operating conditions are measured.