WO1997045953A1 - Method and apparatus for dynamic automatic gain control when pilot signal is lost - Google Patents

Method and apparatus for dynamic automatic gain control when pilot signal is lost Download PDF

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Publication number
WO1997045953A1
WO1997045953A1 PCT/US1997/009233 US9709233W WO9745953A1 WO 1997045953 A1 WO1997045953 A1 WO 1997045953A1 US 9709233 W US9709233 W US 9709233W WO 9745953 A1 WO9745953 A1 WO 9745953A1
Authority
WO
WIPO (PCT)
Prior art keywords
signal
gain control
automatic gain
circuit
level
Prior art date
Application number
PCT/US1997/009233
Other languages
English (en)
French (fr)
Inventor
Stephan W. Vogt
Original Assignee
Scientific-Atlanta, Inc.
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Scientific-Atlanta, Inc. filed Critical Scientific-Atlanta, Inc.
Priority to BR9709377A priority Critical patent/BR9709377A/pt
Priority to AU31495/97A priority patent/AU3149597A/en
Priority to EP97926820A priority patent/EP0903010B1/en
Priority to DE69702520T priority patent/DE69702520T2/de
Publication of WO1997045953A1 publication Critical patent/WO1997045953A1/en

Links

Classifications

    • HELECTRICITY
    • H03ELECTRONIC CIRCUITRY
    • H03GCONTROL OF AMPLIFICATION
    • H03G3/00Gain control in amplifiers or frequency changers
    • H03G3/005Control by a pilot signal
    • HELECTRICITY
    • H03ELECTRONIC CIRCUITRY
    • H03GCONTROL OF AMPLIFICATION
    • H03G3/00Gain control in amplifiers or frequency changers
    • H03G3/20Automatic control
    • H03G3/30Automatic control in amplifiers having semiconductor devices

Definitions

  • the present invention relates to an automatic gain control circuit in a
  • the instant invention is directed to an automatic gain
  • control circuit in a cascaded telecommunication system having a circuit that takes over control of the gain of the automatic gain control circuit when a reference carrier, normally used to control the gain, is lost or falls below a predetermined threshold level.
  • the telecommunication system e.g. , a twisted pair, a coaxial cable, or an optical filter
  • Telecommunication systems typically employ a large number of items of equipment
  • the useful signal in a transmission link may be
  • cable attenuation also varies with temperature. Many other factors may be
  • AGC AGC amplifier
  • pilot signal At receiving stations, or signal-repeating stations, or other distribution points along the telecommunication signal distribution system, the pilot signal is extracted and measured. A signal, representative of the difference between the
  • amplitude of the received pilot signal and a predetermined reference level is used to control the gain of the amplifier to keep the gain of the system at a given, relatively constant, level. Accordingly, as the carrier varies, the gain and slope of the amplifier will vary in proportion.
  • pilot signals to determine gain for a given automatic gain control circuit. For example, if there is a loss of pilot signal, or the level of the pilot becomes too low for detection, the gain levels will tend to maximize with a risk of saturating components located downstream of the detected
  • the present invention provides an improved automatic gain control method
  • the present invention provides a signal that approximates the attenuation of a given
  • the transmission medium based on the temperature of the housing in which the automatic gain control circuit is located.
  • control element of the system will generate an approximated signal based on a temperature
  • pilot signal is redetected.
  • the automatic gain control circuit monitors for the presence of the pilot carrier. If the pilot carrier level falls below a predetermined threshold,
  • the automatic gain control circuit will automatically switch the input of the gain control
  • circuit of the gain control element e.g. , a Bode circuit, which dynamically controls the gain
  • the gain setting will, therefore, be based on an
  • Another object of the present invention is to provide a thermal control circuit that
  • Yet another object of the present invention is to provide automatic switching between
  • the thermal circuit and the received pilot signal based on the signal level of the received pilot
  • an automatic gain control circuit including: a gain element controlling
  • a gain of the automatic gain control circuit a detector for detecting a pilot signal; a comparator
  • the switch is activated when the output of the comparator indicates that a level of the
  • thermal circuit connected to the gain control element via the switch, the thermal circuit providing a signal representing the temperature of a housing in which the automatic gain
  • the gain control circuit is disposed, the gain control circuit providing an attenuation characteristic of
  • the signal provided by the thermal circuit is used by the gain element in place of the pilot
  • the gain control element controlling a gain of the automatic gain control circuit based on a
  • Attenuation approximation signal representing an approximation of attenuation of the
  • FIG. 1 is a block diagram of an AGC portion of a telecommunication distribution
  • FIG. 2 is a schematic diagram of details of a preferred embodiment of the present
  • FIG. 3 is a flow chart representing the steps of the preferred embodiment of the
  • AGC automatic gain control
  • the pilot signal portion of the received signal is received at the input to the amplifier 5.
  • Bode circuit 7 acts as the gain control element of the automatic
  • Bode circuits are well known to those skilled in the art. Typically, a
  • Bode circuit is a tilt network that simulates cable performance over temperature variation, e.g. ,
  • the pivot point of a Bode circuit is usually
  • the Bode circuit 7 drives a second amplification stage 11 that provides an output signal having a level adjusted in accordance with the parameters of the system, i.e. , either a
  • the optional status monitor 13 may also receive a signal 12 from the thermal circuit
  • the status monitor 13 may then
  • the thermal control circuit 2 monitors for the presence of a pilot signal.
  • a band-pass filter 30 receives
  • the pass band of the band pass filter 30 is chosen such that it passes
  • the thermal circuit 2 includes a detector 17, typically
  • the detector 17 is amplified by a DC amplifier 19 and transmitted to a DC switch 21.
  • the pilot signal is also transmitted from the detector 17 to a comparator 25.
  • comparator 25 compares the pilot signal level to a predetermined reference level, V ⁇ f , selected
  • a switch driver 27 is activated and provides a signal to the DC switch 21 , causing
  • thermal circuit 29 is a temperature-sensing circuit, typically
  • thermistor that produces a voltage proportional to the housing temperature of the
  • Bode circuit 29 is directed to the Bode circuit 7 via the switch 21 and the Bode driver 23.
  • Bode circuit 7 provides an approximation of signal attenuation over temperature of a given
  • Bode circuit 7 bases its
  • the automatic gain control circuit may optionally include a manual switch 31 that can
  • the manual switch 31 allows arbitrary switching
  • Figure 3 is a flow diagram outlining the
  • the sampled output from the main amplifier output is attenuated and
  • a DC amplifier 19 is used
  • Temperature-sensing circuit 29 produces a voltage proportional to the housing temperature at
  • Comparator 25 compares the detected level of the pilot signal at point 6 with a
  • the manual switch 31 at point 12 is for testing and alignment purposes.
  • the signal at point 12 is applied to the Bode driver 23 to provide the current necessary to drive
  • the system monitors the input signal for
  • pilot signal is then compared to an arbitrary reference
  • the pilot is either missing or has been attenuated to an unacceptably low level. If the
  • pilot signal level is greater than the reference level, the pilot signal is used to drive the Bode
  • comparator 25 causes the switch driver 27 to signal the DC switch 21 , thus causing the switch
  • Bode circuit 7 provides a signal having an attenuation based on a temperature of the housing
  • the approximation signal is used by

Landscapes

  • Control Of Amplification And Gain Control (AREA)
  • Cable Transmission Systems, Equalization Of Radio And Reduction Of Echo (AREA)
PCT/US1997/009233 1996-05-31 1997-05-30 Method and apparatus for dynamic automatic gain control when pilot signal is lost WO1997045953A1 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
BR9709377A BR9709377A (pt) 1996-05-31 1997-05-30 Método e aparelho para controle de ganho automático dinâmico quando o sinal piloto e perdido
AU31495/97A AU3149597A (en) 1996-05-31 1997-05-30 Method and apparatus for dynamic automatic gain control when pilot signal is lost
EP97926820A EP0903010B1 (en) 1996-05-31 1997-05-30 Method and apparatus for dynamic automatic gain control when pilot signal is lost
DE69702520T DE69702520T2 (de) 1996-05-31 1997-05-30 Verfahren und vorrichtung zur automatischen verstärkungsregelung bei verlorenem pilotsignal

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US08/651,651 1996-05-31
US08/651,651 US5742202A (en) 1996-05-31 1996-05-31 Method and apparatus for dynamic automatic gain control when pilot signal is lost

Publications (1)

Publication Number Publication Date
WO1997045953A1 true WO1997045953A1 (en) 1997-12-04

Family

ID=24613669

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US1997/009233 WO1997045953A1 (en) 1996-05-31 1997-05-30 Method and apparatus for dynamic automatic gain control when pilot signal is lost

Country Status (7)

Country Link
US (1) US5742202A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
EP (1) EP0903010B1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
AU (1) AU3149597A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
BR (1) BR9709377A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
DE (1) DE69702520T2 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
ES (1) ES2151278T3 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
WO (1) WO1997045953A1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7373272B2 (en) * 2006-07-26 2008-05-13 Honeywell International, Inc. Temperature compensated resonant transmission line sensor

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2921267A (en) * 1950-08-02 1960-01-12 Int Standard Electric Corp Protection against failure of pilot wave in carrier communication systems
US3781703A (en) * 1972-10-06 1973-12-25 Jerrold Electronics Corp Electronic amplifier with dual automatic slope control

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2269408A (en) * 1940-09-14 1942-01-06 Bell Telephone Labor Inc Gain control circuits
US2326871A (en) * 1942-01-28 1943-08-17 Bell Telephone Labor Inc Gain control
GB693255A (en) * 1951-04-12 1953-06-24 Automatic Telephone & Elect Improvements in or relating to carrier current transmission systems
BE511542A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) * 1951-05-21
BE511541A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) * 1951-05-21
DE1078624B (de) * 1959-03-17 1960-03-31 Siemens Ag Pilotgesteuerte Pegelregelung fuer ein elektrisches Nachrichtenuebertragungssystem
US3328716A (en) * 1963-09-03 1967-06-27 Automatic Elect Lab Gain regulation circuit utilizing electrochemical memory means in variolosser control circuit
US3510793A (en) * 1964-02-26 1970-05-05 Int Standard Electric Corp Amplifier regulator employing an electrolytic variable resistance device
BE662030A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) * 1964-05-04 1965-10-05
AU407352B2 (en) * 1965-12-29 1970-10-15 Improvements in automatic gain regulators
US3569869A (en) * 1968-06-21 1971-03-09 Walter O Sutton Jr Thermal compensation for a radio frequency transmission line
SE345180B (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) * 1971-06-21 1972-05-15 Ericsson Telefon Ab L M
DE2151794C3 (de) * 1971-10-18 1975-04-24 Standard Elektrik Lorenz Ag, 7000 Stuttgart Anordnung zur Unterdrückung von Regelschwingungen bei einem Trägerfrequenzsystem
GB1435563A (en) * 1972-05-19 1976-05-12 Siemens Ag Repeater amplifiers
US4030034A (en) * 1976-01-30 1977-06-14 General Electric Company Overdrive protection circuit for power line carrier systems and the like
FR2371827A1 (fr) * 1976-11-23 1978-06-16 Cit Alcatel Regulateur a action continue
FR2398344A1 (fr) * 1977-07-21 1979-02-16 Cit Alcatel Regulateur de niveau par onde pilote
US4746876A (en) * 1986-12-22 1988-05-24 Northern Telecom Limited Attenuator control arrangements
JPH05102872A (ja) * 1991-10-07 1993-04-23 Nippon Telegr & Teleph Corp <Ntt> 自動レベル調整回路
JP3052162B2 (ja) * 1991-10-24 2000-06-12 日本無線株式会社 屋外受信装置の異常監視装置

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2921267A (en) * 1950-08-02 1960-01-12 Int Standard Electric Corp Protection against failure of pilot wave in carrier communication systems
US3781703A (en) * 1972-10-06 1973-12-25 Jerrold Electronics Corp Electronic amplifier with dual automatic slope control

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See also references of EP0903010A4 *

Also Published As

Publication number Publication date
US5742202A (en) 1998-04-21
AU3149597A (en) 1998-01-05
BR9709377A (pt) 1999-08-10
EP0903010A4 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) 1999-04-07
DE69702520D1 (de) 2000-08-17
DE69702520T2 (de) 2001-04-19
EP0903010B1 (en) 2000-07-12
EP0903010A1 (en) 1999-03-24
ES2151278T3 (es) 2000-12-16

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