Automatic slope and gain (ASG) detector technique including a pilot signal
AssigneeArris International, Inc.
InventorsJames Farmer, John J. Kenny, John S. Hollabaugh, Calvin W. Stover
Life of this patent
Estimating the term…
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AssigneeArris International, Inc.
InventorsJames Farmer, John J. Kenny, John S. Hollabaugh, Calvin W. Stover
Estimating the term…
An apparatus (7) for switching from a first pilot signal and a second pilot signal on a system transporting a plurality of signals. A tuner (30) receives the signals and provides an output signal to a loop compensation circuit (26). The tuner includes a bandpass filter (22) for removing signals other than the selected pilot signal from the output of the tuner. The output of the bandpass filter is provided to a detector circuit (24, 25). The output of the detector is compared with a reference signal (28) by the loop compensation circuit (28). A microcontroller (39) sends a tuning command to the tuner which causes the tuner to switch from tuning to the first pilot signal to tuning to the second pilot signal and also sends a new reference voltage to the loop compensation circuit. Thus, if the input signal changes from analog to digital modulation on the pilot channel, the set-point, or target level of the reference signal, will automatically change to provide the correct value for operation of the circuit. The microcontroller may change the selected pilot signal based upon a command in the input signal or upon an operator command, such as by setting a switch (not shown).
An ASG system which utilizes a pilot signal and a tuner for maintaining ASG control for a system operable to transport a plurality of station signals, said ASG system comprising:
A method of maintaining ASG control utilizing a pilot signal and a tuner for a system operable to transport a plurality of station signals, said method comprising:
An ASG system for obtaining a pilot signal for a system operable to transport a plurality of station signals, said system having a tuner utilized to adjust the frequency gain of said pilot signal, said ASG system comprising:
Dependencies are inferred from the claim text.