Digital automatic gain controller for satellite transponder

• US 5,687,195 A
• Filed: 06/01/1995
• Issued: 11/11/1997
• Est. Priority Date: 12/16/1994
• Status: Expired due to Term

• Current Assignee: Electronics and Telecommunications Research Institute, Korea Telecommunication Authority
• Original Assignee: Electronics and Telecommunications Research Institute, Korea Telecommunication Authority
• Inventors: Mo, Seung Kee, Kim, Nam Tae, Park, Kwang Rang, Hwang, Yun Son
• Primary Examiner(s): TSE, YOUNG TOI
• Application Number:
  US08/457,504
• Time in Patent Office: 894 Days
• Field of Search: 375/344, 375/345, 455/13.4, 455/13.6, 455/234.1, 455/234.2, 455/249.1, 455/250.1, 455/252.1, 342/92
• US Class Current: 375/345
• CPC Class Codes: H03G 3/001 Digital control of analog signals

Abstract

A digital automatic gain controller for a satellite transponder, comprising an amplification circuit for amplifying a radio frequency signal detected by a detector diode by a difference between the detected radio frequency signal and a temperature compensation signal, a microprocessor for inputting an output signal from the amplification circuit and outputting the inputted signal as a telemetry signal to the earth control station, the microprocessor adjusting an output level of a radio frequency channel in response to a telecommand signal from the earth control station based on the telemetry signal, and a conversion circuit for converting an output data signal from the microprocessor into a drive current for driving a PIN diode attenuator. According to the present invention, the digital automatic gain controller is capable of performing an automatic gain control operation flexibly and reliably on the basis of a program.

Claims

1. A digital automatic gain controller for a satellite transponder, comprising:

amplification means for amplifying a radio frequency signal detected by a detector diode of an output level controller by a difference between the detected radio frequency signal and a temperature compensation signal;

control means for inputting an output signal from said amplification means and outputting the inputted signal as a telemetry signal to an earth control station, said control means adjusting an output level of a radio frequency channel in response to a telecommand signal from said earth control station based on the telemetry signal; and

conversion means for converting the adjusted output level of the radio frequency channel from said control means into a drive current for driving a PIN diode attenuator of the output level controller, wherein an output of the PIN diode attenuator is amplified and inputted into the detector diode through a filter.

2. A digital automatic gain controller for the satellite transponder, as set forth in claim 1, wherein said amplification means includes:

a temperature compensator for generating the temperature compensation signal; and

a video amplifier for amplifying the radio frequency signal detected by said detector diode by the difference between the detected radio frequency signal and the temperature compensation signal from said temperature compensator.

3. A digital automatic gain controller for the satellite transponder, as set forth in claim 1, wherein said control means includes:

an analog/digital converter for converting the output signal from said amplification means into a digital signal and outputting the digital signal as the telemetry signal to said earth control station; and

a memory for outputting a data signal for adjustment of the output level of the radio frequency channel in response to the telecommand signal from said earth control station based on the telemetry signal.

4. A digital automatic gain controller for the satellite transponder, as set forth in claim 3, wherein said control means is an Intel 80C96 series central processing unit.

5. A digital automatic gain controller for the satellite transponder, as set forth in claim 1, wherein said conversion means includes:

a digital/analog converter for converting the adjusted output level of the radio frequency channel from said control means into an analog signal;

a current/voltage converter for converting an output signal from said digital/analog converter into a voltage; and

a voltage/current converter for converting an output voltage from said current/voltage converter into the drive current for driving said PIN diode attenuator.

6. A digital automatic gain controller for the satellite transponder, as set forth in claim 1, further comprising:

address latch means for latching an address signal from said control means; and

data drive means for transferring the adjusted output level of the radio frequency channel from said control means to said conversion means in response to an output signal from said address latch means.