Method for characterizing a transmitting antenna of a satellite in orbit and associated system

• US 9,065,529 B2
• Filed: 09/06/2013
• Issued: 06/23/2015
• Est. Priority Date: 09/07/2012
• Status: Active Grant

• Current Assignee: Thales SA
• Original Assignee: Thales SA
• Inventors: Tessandori, Stephane
• Primary Examiner(s): Rego, Dominic E
• Application Number:
  US14/020,514
• Publication Number:
  US 20140073239A1
• Time in Patent Office: 655 Days
• Field of Search: 455/3.03, 455/12.1, 455/13.2, 455/98, 455/427, 455/404.1, 455/404.2, 455/456.1, 455/9, 701/213, 244/158.1, 244/158.4, 244/158.6
• US Class Current: 1/1
• CPC Class Codes: H04B 7/185 Space-based or airborne stations; Stations for satellite systemsH04B7/204 takes precedence
• CPC Class Codes: H04B 7/1851 Systems using a satellite or space-based relay H04B7/18508, H04B7/18521 take precedence; providing specific services H04B7/18523 - H04B7/18576
• CPC Class Codes: H04B 7/18513 Transmission in a satellite or space-based system
• CPC Class Codes: H04B 7/18519 Operations control, administration or maintenance

Abstract

A method for characterizing a transmitting antenna of a satellite in orbit comprising a payload comprising signal amplification means, includes: configuring the said amplification means to generate thermal noise at the input of the transmitting antenna; acquiring, by means of a ground station, the signal transmitted by the transmitting antenna on the downlink of the satellite over a predetermined time period; during the said predetermined time period, controlling the said satellite in orbit in order to impart on it an angular bias of predetermined variation and recording this variation; correlating the measurement of the signal transmitted on the downlink and the variation of angular bias of the satellite in order to derive therefrom the gain variations of the transmitting antenna as a function of the angular bias of the satellite.

Claims

1. A method for characterizing a transmitting antenna of a satellite in orbit comprising a payload comprising signal amplification means, the method comprising:

configuring the said amplification means to generate thermal noise at the input of the transmitting antenna,

acquiring, by means of a ground station, the signal transmitted by the transmitting antenna on the downlink of the satellite over a predetermined time period,

during the said predetermined time period, controlling the said satellite in orbit in order to impart on it an angular bias of predetermined variation and recording this variation, and

correlating the measurement of the signal transmitted on the downlink and the variation of angular bias of the satellite in order to derive therefrom the gain variations of the transmitting antenna as a function of the angular bias of the satellite.

2. The characterizing method according to claim 1, wherein the said amplification means are configured to operate at saturation.

3. The characterizing method according to claim 1, wherein the said amplification means comprise a first intermediate amplification means and a second high power amplification means, the said intermediate amplification means being configured to amplify the signal to a predetermined level at the input of the second high power amplification means, the said level being determined so that the level of the output signal of the second high power amplification means is higher than the noise level generated by the antenna of the ground station.

4. The characterizing method according to claim 1, wherein the payload comprises at least one receiving antenna and a reception channel and wherein the reception channel is disconnected from the receiving antenna in order to limit the influence of the noise coming from the uplink of the satellite.

5. A system for characterizing a transmitting antenna of a satellite in orbit comprising a payload comprising signal amplification means, the system comprising:

means for configuring the said amplification means in order to generate thermal noise at the input of the transmitting antenna,

means for acquiring the signal transmitted by the transmitting antenna on the downlink of the satellite over a predetermined time period,

means for controlling the satellite in orbit, during the said predetermined time period, in order to impart on it an angular bias of predetermined variation and means of recording this variation, and

means for correlating the measurement of the signal transmitted on the downlink and the variation of angular bias of the satellite in order to derive therefrom the gain variations of the transmitting antenna as a function of the angular bias of the satellite.