WO1986000476A1 - Rf amplifier with frequency spectrum control - Google Patents

Rf amplifier with frequency spectrum control Download PDF

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Publication number
WO1986000476A1
WO1986000476A1 PCT/US1985/001153 US8501153W WO8600476A1 WO 1986000476 A1 WO1986000476 A1 WO 1986000476A1 US 8501153 W US8501153 W US 8501153W WO 8600476 A1 WO8600476 A1 WO 8600476A1
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WO
WIPO (PCT)
Prior art keywords
amplifier
amplitude
signals
input
output
Prior art date
Legal status (The legal status 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 status listed.)
Ceased
Application number
PCT/US1985/001153
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English (en)
French (fr)
Inventor
Gene A. Wagner
Irwin L. Newberg
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Raytheon Co
Original Assignee
Hughes Aircraft Co
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 Hughes Aircraft Co filed Critical Hughes Aircraft Co
Priority to DE8585903168T priority Critical patent/DE3583860D1/de
Publication of WO1986000476A1 publication Critical patent/WO1986000476A1/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S7/00Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
    • G01S7/02Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00
    • G01S7/023Interference mitigation, e.g. reducing or avoiding non-intentional interference with other HF-transmitters, base station transmitters for mobile communication or other radar systems, e.g. using electro-magnetic interference [EMI] reduction techniques
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S7/00Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
    • G01S7/02Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00
    • G01S7/28Details of pulse systems
    • G01S7/282Transmitters
    • HELECTRICITY
    • H03ELECTRONIC CIRCUITRY
    • H03CMODULATION
    • H03C1/00Amplitude modulation
    • H03C1/02Details
    • H03C1/06Modifications of modulator to reduce distortion, e.g. by feedback, and clearly applicable to more than one type of modulator

Definitions

  • This invention relates generally to RF amplifiers and, more particularly, to an RF amplifier arrangement for providing output signals having a controlled or modified frequency distribution.
  • the subject invention provides for amplitude control of the input signals to an RF amplifier so as to provide a predetermined variation in the output power of the amplifier, which variation causes a desired modification in the output frequency spectrum of the amplifier's output signal.
  • a computer controlled feedback loop is employed to provide the amplitude control of the amplifier's output signals and phase control is also implemented by means of a feedback loop.
  • One such embodiment comprises an RF amplifier and circuit means for adjusting the amplitude and phase of the input signals to the amplifier as a function of the amplitude and phase, respectively, of the output signals from the amplifier and for also adjusting the amplitude of the input signals so as to cause the power of the output signals to vary in accordance with the predetermined sequence whereby such amplitude control of the input signals results in a modified frequency distribution in the energy of the output signals.
  • the circuit means may include a source of RF signals, a controllable power adjustment device coupled to receive a portion of the output power from the RF amplifier, computer means programmed to control the relative response of the power adjustment device in accordance with the predetermined sequence and modulators coupled between the output of the RF signal source and the input of the amplifier for adjusting the phase and amplitude of the input signal as a function of the phase and amplitude, respectively, of the output signal from the power adjustment device.
  • One embodiment of the invention further comprises means for measuring the output power of the RF amplifier and the computer means includes an arrangment for scanning the controllable power adjustment device over a range of values and for storing the resultant parameters that produce the RF output power levels of the predetermined sequence.
  • FIG. 1 is a block diagram of an RF amplifier arrangement in accordance with the subject invention wherein the frequency spectrum of the output signal from the RF amplifier is controlled by means of amplitude control of the amplifier's input signal;
  • FIG. 2 illustrates an amplitude weighted pulse having Dolph-Chebychev weighting which is associated with 45 dB sidelobe levels;
  • FIG. 3 illustrates the expected frequency spectrum of the output signal for the RF amplifier arrangement of FIG. 1;
  • FIG. 4 is a typical spectrum of the output signals from a pulsed transmitter without waveform amplitude control
  • FIG. 5 is an arrangement similar to that of FIG. 1 with the addition of means for measuring and storing the control signal values associated with preselected output power levels;
  • FIG. 6 is an RF amplifier arrangement similar to that of FIG. 1 except that amplitude control of the input signal is provided by open loop computer control of the input signal to the RF amplifier;
  • FIG. 7 is an arrangement similar to that of
  • FIG * .6 except that feedback phase control of the input signal to the RF amplifier has not been implemented.
  • FIG. 8 is a block diagram of an RF amplifier arrangement which implements amplitude control of the amplifier's input signals for the situation in which two carrier frequencies are simultaneosly processed.
  • the frequency spectrum controlled RF amplifier arrangement there shown includes an RF source 10, a directional coupler 12, phase and amplitude modulators 14, and 16, respectively, and an RF power amplifier 18.
  • the output signal from amplifier 18 is applied to a utilization device such as a radar antenna (not shown) and a sample thereof is applied through a directional coupler 20 to a voltage controlled attenuator 22.
  • the amount of attenuation applied by voltage controlled attenuator 22 is determined by signals applied from a computer 24 to the control input of attenuator 22.
  • the computer is programmed so as to provide a predetermined sequence of weighting function parameters.
  • An amplitude detector 28 and amplitude modulator 16 are part of a feedback loop which operates to maintain the input signal to amplitude detector 26 at a constant power level. Therefore, the output power from amplifier 18 can be controlled and shaped by controlling the attenuation provided by the voltage controlled attenuator 22. Hence, the shape of the output signal from the RF amplifier 18 is determined by the control signals applied to attenuator 22 from the computer 24. As noted hereinabove, and as shown in FIGS. 3 and 4, amplitude control of the RF outputs pulses translates into modification of the frequency spectrum of these pulses.
  • An example of a set of weighting function parameters is illustrated in FIG. 2 for Dolph-Chebychev weights for 45 dB sidelobes.
  • FIG. 3 shows the resulting spectrum for such a weighted waveform which has a 300 Hz pulse repetition frequency, a center frequency of 9.8 GHz, step width of 26 micro ⁇ seconds and a duty factor of 0.125.
  • the vertical scale is 10 dB per division and the horizontal scale is 5.0 kHZ' per division.
  • FIG. 4 shows the spectrum of a similar pulsed waveform without amplitude weighting
  • Table I shows Dolph-Chebychev amplitude weights for 35 dB, 40 dB, 45 dB and 50 dB sidelobes. Since the RF amplifiers are generally not linear devices the values of attenuation command signals are derived from a set of prior measurements made on the amplifier arrangement. For example, the maximum output power level is selected and assigned the value "1.000" and then the input signal to attenuator 22 is adjusted until the power represented by the respective steps shown in FIG. 2 and Table I are obtained and then computer 24 is programmed accordingly.
  • the RF output amplifier is sometimes operated in satura ⁇ tion to minimize AM noise from both the input drive source and the amplifier itself.
  • the amplifier 18 since output signal amplitude signal control is effected by controlling the input signal, the amplifier 18 must be operated below saturation; however, acceptable AM noise levels are obtained by means of the amplitude feedback loop which includes the detector 28 and modulator 16.
  • phase variations can be expected, for example, with variations in output power and from the operation of attenuator 22.
  • the phase feedback loop which includes a phase detector 30 and phase modulator 14 reduces such phase variations.
  • phase detector 30 One input to phase detector 30 is applied from RF source 10 through direc ⁇ tional coupler 12 and the other input is applied from voltage controller attenuator 22 through a directional coupler 26 ⁇
  • Microwave Associates Part No. MPM 371 includes a stripline phase modulator (0 to 60°) and an amplitude modulator (0 to 50 dB)
  • Part No. MPM 372 includes a 4-bit phase shifter, a phase detector and an amplutide detector
  • Part No. MPM 373 is a voltage controlled attenuator.
  • Phase modulator 14 may comprise the combination of the 4-bit digital phase shifter and the stripline continuous phase shifter with suitable control electronics to step the 4-bit phase shifter so as to maintain the loop within the control range of the stripline continuous phase shifter.
  • An example of a system which uses feedback loops to reduce undesirable modulation components in a microwave power amplifier is presented in U.S. Patent No. 4,134,114 to Riggs et al and is entitled "Radar System Having Amplitude and Phase Modulation and Demodulation".
  • computer 24 provides gate control signals to RF amplifier 18, which may be a gated TWT, for example, so as to turn the amplifier off between output signal pulses.
  • the computer may control a diode switch (not shown) disposed between modulators 14 and 16, for example, to accomplish the gating function, or both methods may be used to implement improved gating.
  • FIG. 5 The configuration of FIG. 5 is similar to that of ° FIG. 1 with the addition of a power monitor 32 coupled through directional coupler 34 so as to receive a sample of the RF output power from RF power amplifier 18.
  • Computer 24 is programmed so that during a calibration mode of operation voltage controlled attenuator 22 is 5 scanned over a predetermined range of attenuation values and the control parameter (control signals to 22) values and resultant power levels values are stored and tabulated. Then during operation the parameter values for the preselected desired power level sequence 0 (weighting factors) are used.
  • Such a calibration update mode may be run on a programmed schedule or by operator command.
  • FIG. 6 The embodiment of FIG. 6 is similar to that of FIG. 1 except that the amplitude control is performed 5 "open loop" by attenuator 22 under control of computer 24.
  • the computer uses a table of attenuation values from a computer memory to set attenuator 22 so as to obtain the desired output power.
  • Phase control is maintained by a feedback loop which includes phase 0 modulator 14 and phase detector 30. It is noted that phase control can reduce frequency modulation (FM) noise which may be the higher noise source in a transmitter's output, i.e., higher than AM noise.
  • FM frequency modulation
  • FIG. 7 The arrangement of FIG. 7 illustates the basic concept of frequency spectrum control by control of the input signal to the power amplifier 18.
  • Computer 24 uses a table of attenuation values from a computer memory to control attenuator 22.
  • an arrangement which uses pulsed input signals having different carrier frequencies can also be implemented. If the pulses are overlapped in the time domain (pulses are partially time coincident) then separate feedback loops would be used to control each input signal channel; this is shown in FIG. 8 for two frequencies. As there shown, signals which have a carrier frequency FI are provided for a first signal channel by RF source 10 and signals which have a carrier frequency F2 are provided for a second signal channel by a RF source 10*.
  • the two feedback loops shown in FIG. 8 each operate in a manner similar to that described herein above relative to FIG. 1.
  • the loops respond to the appropriate respective frequencies due to filter 38 and 38' which applies feedback signals for control of the FI and F2 signal channels respectively.
  • the output signal sample from directional coupler 20 is applied to a coupler 36 and two output signals therefrom are applied as respective inputs to filters 38 and 38*.
  • the amplitude and phase controlled signals from amplitude modulator 16 and 16' are combined by coupler 40 and applied as a combined input signal to RF amplifier 18.
  • Computer 24 controls the attenuation of voltage controlled attenuators 22 and 22' in the manner described herein above relative to FIG. 1.
  • the amplitude weighting functions need not be the same for both signal channels; for example, computer 24 may be programmed to apply the 35 db sidelobe level weights (see Table I) to the signals, for the FI channel and 45 db sidelobe level weights to the signals for the F2 channel. It is noted that the multiple carrier frequency implementation reduces loss of average power capability associated with the input signal amplitude contol technique since the variation in peak power output during the overlap time is less than the peak power variation for weighted waveforms having no overlap.

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  • Engineering & Computer Science (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Amplifiers (AREA)
  • Amplitude Modulation (AREA)
  • Radar Systems Or Details Thereof (AREA)
  • Digital Transmission Methods That Use Modulated Carrier Waves (AREA)
  • Cable Transmission Systems, Equalization Of Radio And Reduction Of Echo (AREA)
PCT/US1985/001153 1984-06-28 1985-06-18 Rf amplifier with frequency spectrum control Ceased WO1986000476A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE8585903168T DE3583860D1 (de) 1984-06-28 1985-06-18 Hf-verstaerker mit steuerung des frequenz-spektrums.

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US626,098 1984-06-28
US06/626,098 US4600892A (en) 1984-06-28 1984-06-28 RF amplifier with frequency spectrum control

Publications (1)

Publication Number Publication Date
WO1986000476A1 true WO1986000476A1 (en) 1986-01-16

Family

ID=24508933

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US1985/001153 Ceased WO1986000476A1 (en) 1984-06-28 1985-06-18 Rf amplifier with frequency spectrum control

Country Status (6)

Country Link
US (1) US4600892A (enExample)
EP (1) EP0190166B1 (enExample)
JP (1) JPS61502580A (enExample)
DE (1) DE3583860D1 (enExample)
IL (1) IL75515A (enExample)
WO (1) WO1986000476A1 (enExample)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1987004305A1 (en) * 1985-12-30 1987-07-16 Hughes Aircraft Company Traveling wave tube drive controller
WO2001065685A1 (de) * 2000-03-03 2001-09-07 Siemens Aktiengesellschaft Verfahren und sendeschaltung zur erzeugung eines sendesignals
US20180031687A1 (en) * 2016-08-01 2018-02-01 Vega Grieshaber Kg Radar fill level measurement device

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IT1215370B (it) * 1987-02-26 1990-02-08 Gtg Ora Siemens Telecomunicazi Linearizzatore per amplificatore di potenza a microonde.
FR2639775A1 (fr) * 1988-11-25 1990-06-01 Thomson Csf Dispositif de correction de phase induite par le fonctionnement en classe c de l'amplificateur " etat solide " et chaine radar utilisant un tel dispositif
JPH03198512A (ja) * 1989-12-27 1991-08-29 Mitsubishi Electric Corp 高周波増幅器
GB9002789D0 (en) * 1990-02-08 1990-04-04 Marconi Co Ltd Circuit for reducing distortion produced by an r.f.power amplifier
US5101173A (en) * 1990-11-28 1992-03-31 The United States Of America As Represented By The Secretary Of The Air Force Stored program controlled module amplifier bias and amplitude/phase compensation apparatus
US5101211A (en) * 1991-01-10 1992-03-31 Hughes Aircraft Company Closed loop RF power amplifier output correction circuit
US5175879A (en) * 1991-04-25 1992-12-29 Motorola, Inc. Linear amplifier with feedback path and phase error compensation
US5365190A (en) * 1993-05-03 1994-11-15 Duly Research, Inc. Feed-forward digital phase and amplitude correction system
FI105609B (fi) * 1998-10-27 2000-09-15 Nokia Mobile Phones Ltd Menetelmä ja järjestely lähetyssignaalin muodostamiseksi
US6285255B1 (en) * 1999-11-02 2001-09-04 Harris Corporation Adaptive compensation for carrier signal phase distortion
US6459337B1 (en) 2000-07-05 2002-10-01 Teledyne Technologies Incorporated System and method for noise and spurious suppression in power amplifier systems
US6650875B1 (en) * 2000-08-30 2003-11-18 Skyworks Solutions, Inc. Transmitter architecture having a secondary phase-error correction loop including an amplitude reconstruction system
US6535060B2 (en) 2000-12-05 2003-03-18 Teledyne Technologies Incorporated System and method for noise and spurious supression in power amplifier systems
GB0030693D0 (en) 2000-12-15 2001-01-31 Nokia Mobile Phones Ltd Amplifier circuit radio transmitter method and use
US6498532B2 (en) 2001-01-12 2002-12-24 Teledyne Technologies Incorporated System and method for linearizing vacuum electronic amplification
JP4772232B2 (ja) * 2001-08-29 2011-09-14 アジレント・テクノロジーズ・インク 高周波増幅回路及び高周波増幅回路の駆動方法
US6734734B2 (en) 2002-07-24 2004-05-11 Teledyne Technologies Incorporated Amplifier phase droop and phase noise systems and methods
US6892057B2 (en) * 2002-08-08 2005-05-10 Telefonaktiebolaget Lm Ericsson (Publ) Method and apparatus for reducing dynamic range of a power amplifier
GB2414352A (en) * 2004-05-18 2005-11-23 Roke Manor Research An adaptively-corrected RF pulse amplifier for a beam-steered radar antenna array
US7423464B2 (en) * 2006-04-04 2008-09-09 Johann-Christoph Scheytt Phase and amplitude modulator
US7656236B2 (en) 2007-05-15 2010-02-02 Teledyne Wireless, Llc Noise canceling technique for frequency synthesizer
US8179045B2 (en) 2008-04-22 2012-05-15 Teledyne Wireless, Llc Slow wave structure having offset projections comprised of a metal-dielectric composite stack
US9314648B2 (en) * 2011-12-23 2016-04-19 Texas Tech University System System, method and apparatus for tracking targets during treatment using a radar motion sensor
US9791548B2 (en) * 2012-09-19 2017-10-17 Furuno Electric Co., Ltd. Pulse compression radar
US9784819B2 (en) * 2012-09-19 2017-10-10 Furuno Electric Co., Ltd. Pulse compression radar
US9202660B2 (en) 2013-03-13 2015-12-01 Teledyne Wireless, Llc Asymmetrical slow wave structures to eliminate backward wave oscillations in wideband traveling wave tubes
DE102013111512A1 (de) * 2013-10-18 2015-04-23 Hella Kgaa Hueck & Co. Radargerät und Verfahren zum Betreiben eines Radargerätes

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FR2387547A1 (fr) * 1977-04-14 1978-11-10 Hughes Aircraft Co Radar comportant des circuits de modulation et de demodulation en amplitude et en phase
GB2011741A (en) * 1977-11-30 1979-07-11 Plessey Co Ltd Power amplifier arrangement
DE2835751B1 (de) * 1978-08-16 1979-10-25 Standard Elek K Lorenz Ag HF-Leistungsverstaerker mit einer Modulationseinrichtung
GB2059217A (en) * 1979-09-14 1981-04-15 Int Standard Electric Corp Radar envelope detection system

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Patent Citations (4)

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Publication number Priority date Publication date Assignee Title
FR2387547A1 (fr) * 1977-04-14 1978-11-10 Hughes Aircraft Co Radar comportant des circuits de modulation et de demodulation en amplitude et en phase
GB2011741A (en) * 1977-11-30 1979-07-11 Plessey Co Ltd Power amplifier arrangement
DE2835751B1 (de) * 1978-08-16 1979-10-25 Standard Elek K Lorenz Ag HF-Leistungsverstaerker mit einer Modulationseinrichtung
GB2059217A (en) * 1979-09-14 1981-04-15 Int Standard Electric Corp Radar envelope detection system

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1987004305A1 (en) * 1985-12-30 1987-07-16 Hughes Aircraft Company Traveling wave tube drive controller
US4709215A (en) * 1985-12-30 1987-11-24 Hughes Aircraft Company Traveling wave tube drive controller
WO2001065685A1 (de) * 2000-03-03 2001-09-07 Siemens Aktiengesellschaft Verfahren und sendeschaltung zur erzeugung eines sendesignals
WO2001065683A1 (de) * 2000-03-03 2001-09-07 Siemens Aktiengesellschaft Verfahren und sendeschaltung zur erzeugung eines sendesignals
US6968163B2 (en) 2000-03-03 2005-11-22 Siemens Aktiengesellschaft Method and transmission circuit for generating a transmission signal
US20180031687A1 (en) * 2016-08-01 2018-02-01 Vega Grieshaber Kg Radar fill level measurement device
EP3279619A1 (de) * 2016-08-01 2018-02-07 VEGA Grieshaber KG Radarfüllstandmessgerät
CN107677339A (zh) * 2016-08-01 2018-02-09 Vega格里沙贝两合公司 雷达料位测量装置
US10802127B2 (en) 2016-08-01 2020-10-13 Vega Grieshaber Kg Radar fill level measurement device

Also Published As

Publication number Publication date
JPS61502580A (ja) 1986-11-06
US4600892A (en) 1986-07-15
DE3583860D1 (de) 1991-09-26
IL75515A (en) 1989-01-31
EP0190166A1 (en) 1986-08-13
JPH0479580B2 (enExample) 1992-12-16
EP0190166B1 (en) 1991-08-21

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