Method for operating an amplifier module of a satellite

Patent metadata

Field	Value
Publication number	US-9350307-B2
Application number	US-201414218087-A
Country	US
Kind code	B2
Filing date	Mar 18, 2014
Priority date	Mar 19, 2013
Publication date	May 24, 2016
Grant date	May 24, 2016

Abstract

A method for operating an amplifier module of a communication satellite involves establishing an undesired state of the amplifier module, storing state data, which indicate the undesired state, in a nonvolatile memory of the amplifier module, after the undesired state has been established, and deactivating the amplifier module after the storage of the state data.

First claim

What is claimed is:

1. A method for operating an amplifier module of a communication satellite, the method comprising the steps:
establishing an undesired state of the amplifier module;
storing state data, which indicate the undesired state, in a nonvolatile memory of the amplifier module, after the undesired state has been established;
deactivating the amplifier module after the storage of the state data.

2. The method of claim 1 , wherein the undesired state is established by executing a protective function, which is applied to detected parameters of the amplifier module and which ascertains the undesired state from the detected parameters.

3. The method of claim 2 , wherein the stored state data comprise a type of the protective function.

4. The method of claim 2 , wherein the stored state data comprise values of parameters of the amplifier module, which were processed by the protective function.

5. The method of claim 1 , wherein the stored state data comprise values of parameters of the amplifier module, which were detected before the establishment of the undesired state or were detected before the deactivation of the amplifier module.

6. The method of claim 1 , further comprising the step:
establishing a further undesired state and storing further state data, which relate to the further undesired state, wherein the state data and the further state data are stored together in the nonvolatile memory.

7. The method of claim 1 , further comprising the step:
transmitting the stored state data to a ground station.

8. The method of claim 7 , wherein the stored state data are transmitted when the amplifier module receives a corresponding telecommand from the ground station.

9. The method of claim 7 , wherein the stored state data are automatically transmitted after the amplifier module has been reactivated.

10. The method of claim 7 , wherein the stored state data remain stored in the nonvolatile memory after the transmission to the ground station.

11. An amplifier module for a communication satellite, comprising:
an amplifier unit; and
a controller configured to activate the amplifier unit, wherein the controller comprises a nonvolatile, writable memory configured to store state data of the amplifier module when the amplifier module is not energized by an external power supply,
wherein the controller is configured to
establish an undesired state of the amplifier module;
store state data, which indicate the undesired state, in a nonvolatile memory of the amplifier module, after the undesired state has been established;
deactivate the amplifier module after the storage of the state data.

12. The amplifier module of claim 11 , wherein the controller comprises a telemetry component configured to detect operating parameters or settable parameters of the amplifier module as state data.

13. The amplifier module of claim 11 , wherein the controller comprises a protective function component configured to analyze operating parameters or settable parameters of the amplifier module, to determine an undesired state of the amplifier module.

14. The amplifier module of claim 11 , further comprising:
a telecommand interface configured to receive a telecommand, which triggers a transmission of state data stored in the nonvolatile memory.

15. The amplifier module of claim 11 , wherein the amplifier unit is a traveling wave tube as an amplifier unit.

Assignees

• Tesat Spacecom Gmbh & Co Kg

Inventors

• Katz Hanspeter
• Reinwald Gerhard

Classifications

• H04B17/17

  Detection of non-compliance or faulty performance, e.g. response deviations (H04B17/18 takes precedence) · CPC title

• H04B17/104

  of other parameters, e.g. DC offset, delay or propagation times · CPC title

• H03F3/58 Primary

  using travelling-wave tubes · CPC title

• H04B7/18515

  Transmission equipment in satellites or space-based relays · CPC title

• H04B17/16

  Test equipment located at the transmitter · CPC title