USOO7317894B2
`
`(12) United States Patent
`US 7,317,894 B2
`(10) Patent N0.:
`
`Hirose
`(45) Date of Patent:
`Jan. 8, 2008
`
`[54) SATELLITE DIGITAL RADIO BROADCAST
`RECEIVER
`
`(75)
`
`Inventor: KojiHirose, Setagaya-ku (JP)
`,
`~
`.
`-
`-
`-
`(73) Asslgnee.
`Iggbushlkl Kalsha Kenwood, Tokyo
`(
`)
`,
`.
`.
`.
`.
`(*) Nome:
`SUbJeCFTO any dISCIalmerzthetenn 0mm
`Patent IS extended or adJuSted under 35
`U.S.C. 154(b) by 288 days.
`
`(21) Appl. N0.: 10/781,726
`
`.
`
`6,301,313 B1* 10/2001 Gevargiz et a1,
`............ 375/340
`6,484,042 B1* 11/2002 Loke
`455/2341
`
`.. 455/2452
`6,498,927 B2* 12/2002 Kang et al.
`
`6,510,317 31*
`455/428
`112003 Make eta],
`6,549,774 B1*
`4/2003 Titlebaum et all
`.
`.. 455/427
`
`6,557,029 B2*
`.. 455/131
`4/2003 Szymansky
`
`6,584,090 131*
`612003 Abdelgany et 31’
`455/82
`
`6,735,416 B1*
`. 455/302
`5/2004 lVIaIko et a],
`2001/0022821 A1*
`9/2001 Ichihara
`375/345
`
`200110041532 A1* 11/2001 Tomasz et al.
`4553.02
`
`455/2341
`2002/0025792 A1*
`212002 Isoda
`2004/0229583 A1* 11/2004 Ogino .....
`455/301
`
`6/2005 Coffin, III .................. 455/302
`2005/0124289 A1*
`2007/0004351 A1*
`1/2007 Dekker
`455/1271
`
`(22)
`
`Filed:
`
`Feb. 20, 2004
`
`* cited by examiner
`
`(65)
`
`Prior Publication Data
`
`,
`US 2004-0168193 A1
`
`Aug. 26’ 2004
`
`Primary ExamineriLaua Le
`(74) Attorney, Agent, or FinniEric J. Robinson; Robinson
`Intellectual Property Law Ofiice, PC.
`
`Foreign Application Priority Data
`(30)
`Feb. 26, 2003
`(JP)
`............................. 2003-048572
`
`(57)
`
`ABSTRACT
`
`[51)
`
`Int. Cl-
`(2006.01)
`H04H 1/00
`455/302; 455/2341; 455/2501
`(52) U.S. Cl.
`(58) Field of Classification Search ,,,,,, 4553012302,
`455723417 2321, 272, 277.1, 2772, 226.1,
`455/2262, 67.11, 67.12, 133, 136; 725/68271a
`725/63764
`See application file for complete search history.
`W
`References Clted
`U.S. PATENT DOCUMENTS
`
`(56)
`
`3/1992 LOPer et 3L ~~~~~~~~~~~~~ 455/249-1
`52095.53 A *
`4/ 1994 Nékagawa et 31~
`~~~~~~~~~~~ 725/71
`5 EDI-3? A :
`
`641994 BIISkman
`455/13'1
`5 3195/3 A '
`8/1998 BnSkman """""""""" 455/344
`5’794‘138 A *
`5,966,186 A * 10/1999 Shigihara et al.
`........... 348/570
`6,078,796 A *
`6/2000 Ling ....................... 455/2341
`6,091,931 A *
`7/2000 Ben-Efraim et a1.
`....... 455/302
`
`A satellite digital radio broadcast receiver has an integrated
`circuit including a first reception series for processing a
`satellite wave signal from a satellite and a second reception
`series for processing a ground wave signal from a repeater
`in order to receive both the satellite wave signal and the
`ground wave signal having the same broadcast contents and
`different modulationniethods. The receiver has an automatic
`gain control unit for amplifying a signal from a single
`antenna at a variable gain amplifier, and in accordance with
`the level of a signal outputted from the variable gain
`amplifier,
`for controlling the gain of the variable gain
`amplifier; and a two-way distributor for distributing an
`output of the automatic control unit to two distribution
`outputs, wherein one distribution output of the two-way
`distributor is supplied to the first reception series of the
`integrated circuit and the other distribution output is sup-
`plied to the second reception series of the integrated circuit
`'
`
`2 Claims, 8 Drawing Sheets
`
`
`
`31
`
`
`
`36
`
`INTERMEDIATE FREQUENCY
`DEMODULATION STAGE
`[FOR SATELLITE WAVE]
`
`
`CONTROL
`CIRCUIT
`
`WAVE
`DETECTION
`
`
`
`18
`
`17
`
`INTERMEDIATE FREQUENCY
`DEMODULATIDN STAGE
`[FOR GROUND WAVE]
`28
`
`27
`
`INTEL 1324
`
`N
`
`

`

`U.S. Patent
`
`Jan.8,2008
`
`Sheet170f8
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`US 7,317,894 B2
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`

`U.S. Patent
`
`Jan. 8, 2008
`
`Sheet 2 of 8
`
`US 7,317,894 B2
`
`FIG. 2
`
`
`
` GROUND
`
`

`

`U.S. Patent
`
`Jan.8,2008
`
`Sheet3 0f8
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`US 7,317,894 B2
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`U.S. Patent
`
`Jan. 8, 2008
`
`Sheet 4 of 8
`
`US 7,317,894 B2
`
`FIG. 4
`
`LEVEL
`
`TIME
`
`

`

`U.S. Patent
`
`Jan. 8, 2008
`
`Sheet 5 of 8
`
`US 7,317,894 B2
`
`FIG. 5
`
`
`
`\\
`
`RECEIVED SIGNAL LEVEL OF GROUND WAVE (dBm)
`
`
`
` VSIGNALLEVELOFDISTURBANCEWAVE(dBm)
`
`
`
`
`
`

`

`U.S. Patent
`
`Jan.8,2008
`
`Sheet6 0f8
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`

`

`U.S. Patent
`
`Jan. 8, 2008
`
`Sheet 7 of 8
`
`US 7,317,894 B2
`
`FIG. 7
`
`
`
`
`
`SIGNALLEVELOFDISTURBANCEWAVE(dBm)
`
`RECEIVED SIGNAL LEVEL OF GROUND WAVE (dBm)
`
`

`

`U.S. Patent
`
`Jan.8,2008
`
`Sheet8 0f8
`
`US 7,317,894 B2
`
`FIG. 8
`
`IIl|
`II
`
`III
`III
`
`I!
`II
`ll.-
`
`TIME
`
`

`

`US 7,317,894 B2
`
`1
`SATELLITE DIGITAL RADIO BROADCAST
`RECEIVER
`
`BACKGROUND OF THE INVENTION
`
`1. Field of the Invention
`
`The present invention relates to a satellite digital radio
`broadcast receiver for receiving a broadcast program having
`the same contents but different modulation methods.
`
`2. Related Background Art
`Satellite digital radio broadcasting from a plurality of
`elliptical orbit satellites moving along a so-called figure 8
`orbit is presented, for example, by US SIRIUS Satellite
`Radio Incorporated. The outline of the whole system of
`satellite broadcast is shown in FIG. 1. This broadcast system
`uses one Geo stationary satellite and three elliptical orbit
`satellites (not stationary satellite) each moving along a figure
`8 orbit. Since the service area is the North America, if a Geo
`stationary satellite only is used, the elevation angle of an
`antenna is low so that this is not suitable for mobile stations.
`
`An elliptical orbit satellite moves along the figure 8 orbit so
`that it does not always locate overhead. Therefore, a radio
`broadcast receiver sequentially and alternately receives a
`signal from any two satellites among the three elliptical orbit
`satellites.
`In an area where it is difficult to receive a radio wave from
`
`an elliptical orbit satellite or in an urban area where it is
`difiicult to receive a satellite broadcast radio wave, a radio
`broadcast receiver receives in some cases a radio wave
`
`(ground wave) from a ground repeater which is controlled
`by a Geo stationary orbit satellite. Therefore, the satellite
`radio broadcast receiver receives three radio waves in total,
`two satellite waves and one ground wave, at the same time
`at its wide band RF amplifier. FIG. 2 shows the spectrum of
`radio waves to be received by the receiver. The center
`frequency of this spectrum is approximately 2.3 GHz, and
`the satellite wave and ground wave have both the band width
`of about 4 MHZ. Although the satellite wave #1 and the
`ground wave are received at the same timing, the satellite
`wave #2 is received at
`the timing delayed by several
`seconds, and so time diversity is presented. Of three satellite
`waves from the elliptical orbits, the satellite wave #1 or #2
`is used depending upon their orbits so that the control for the
`time diversity and also fine frequency tuning are carried out.
`In the receiver, a band-pass filter built in the tuner unit
`separates each band, and the received signals are demodu-
`lated, combined and thereafter synthesized through synchro-
`nization.
`
`The features of this satellite digital radio broadcast system
`are summarized as in the following:
`1) Features of Radio Waves
`Since a ground wave has a propagation path different from
`that of a satellite wave, the way how the level fluctuates and
`the like are difierent from those of the satellite wave.
`Since the satellite wave is transmitted from a satellite on
`
`the elliptical orbit, it is received by the receiver at a high
`elevation angle. Since the propagation path does not change
`largely, the satellite wave can be received reliably unless the
`mobile station enters a tunnel or passes under a high way.
`2) Features of Reception System
`The receiver receives three waves containing the same
`contents. However, each radio wave has different frequency
`and propagation path, and a different time period while the
`same data is received. These radio waves are synthesized
`and demodulated so that the effects of frequency diversity,
`space diversity and time diversity can be obtained.
`
`10
`
`15
`
`25
`
`35
`
`40
`
`45
`
`50
`
`Ln Ln
`
`60
`
`65
`
`2
`FIG. 3 shows the structure of a tuner unit of a satellite
`
`digital broadcast receiver 20 of the current system.
`In the tuner having the structure shown in FIG. 3, an
`antenna 11 receives a radio wave signal from a ground
`repeater, i.e., a ground signal, the antenna having the direc-
`tional characteristics matching the ground signal. The band
`of the received signal is limited by a band-pass filter 12, and
`an output of the band-pass filter 12 is selectively supplied
`either to a high frequency amplifier 13 or an attenuator 14 to
`be amplified or attenuated. An antenna 21 receives a radio
`wave signal from a satellite,
`i.e., a satellite signal,
`the
`antenna having the directional characteristics matching the
`satellite signal. The band of the received signal is limited by
`a band-pass filter 22.
`An output signal from the high frequency amplifier 13 or
`an output signal from the attenuator 14 is amplified by a
`variable gain amplifier 15, and an output of this amplifier is
`supplied to a mixer 16 whereat
`it is converted into an
`intermediate frequency easy to be processed. An output of
`the mixer 16 is detected by a detector 17 to obtain a detection
`voltage corresponding to the input signal level. This detec-
`tion voltage is supplied to a control circuit 18 which deter-
`mines a gain of the variable gain amplifier 15 in accordance
`with the supplied detection voltage, to thereby perform an
`automatic gain control (AGC). An output of the mixer 16 is
`also sent as a ground signal to an intemiediate frequency
`stage to be subjected to an intermediate frequency process.
`An output of the intermediate frequency stage is supplied to
`a demodulation stage to be subjected to a demodulation
`process. If the input signal level is judged small from the
`detection voltage, the high frequency amplifier 13 is selected
`by switches 19a and 195, whereas if the input signal level is
`large, the attenuator 14 is selected by the switches 19a and
`19b.
`
`An output signal from the band-pass filter 22 is amplified
`at a variable gain amplifier 25, and an output ofthis amplifier
`is supplied to a mixer 26 whereat it is converted into an
`intermediate frequency easy to be processed. An output of
`the mixer 26 is detected by a detector 27 to obtain a detection
`voltage corresponding to the input signal level. This detec-
`tion voltage is supplied to a control circuit 28 which deter-
`mines a gain of the variable gain amplifier 25 in accordance
`with the supplied detection voltage,
`to thereby perform
`AGC. An output of the mixer 26 is also sent as a satellite
`signal to an intermediate frequency stage to be subjected to
`an intermediate frequency process. An output of the inter-
`mediate frequency stage is supplied to a demodulation stage
`to be subjected to a demodulation process.
`The variable gain amplifiers 15 and 25, mixers 16 and 26,
`detectors 17 and 27 and control circuits 18 and 28 are
`
`fabricated in an integrated circuit IC. There are two series,
`a ground wave signal series including the variable gain
`amplifier 15, mixer 16, detector 17 and control circuit 18,
`and a satellite wave signal series including the variable gain
`amplifier 25, mixer 26, detector 27 and control circuit 28.
`The reason of division into two series is that although the
`broadcast contents are the same, the modulation methods are
`different between the grolmd wave signal of an OFDM
`modulation and the satellite wave signal of a QPSK modu-
`lation, the bands at the succeeding intermediate frequency
`stages are different and the gain distributions are diiferent.
`In the satellite digital radio broadcast receiver described
`above, the frequency of a received satellite wave signal is
`adjacent to that of a received ground wave signal. These two
`signals, the satellite wave reception signal and ground wave
`reception signal, are input to the two series of the tuner.
`Since different gain settings are performed in the integrated
`
`

`

`US 7,317,894 B2
`
`3
`circuit IC of the tuner because of different levels of the
`
`satellite wave reception signal and ground wave reception
`signals and the like, the tuner is divided into the two series
`in the integrated circuit IC.
`The tuner of the satellite digital radio broadcast receiver
`20 receives an adjacent disturbance wave signal b such as
`shown in FIG. 4. In order to process this disturbance signal,
`the switching circuit for switching between the high fre-
`quency amplifier 13 and attenuator 14 is provided at the
`front stage of the integrated circuit IC in the ground wave
`signal reception series. This switching circuit operates in
`response to the output level of the detector 17 provided in
`the integrated circuit IC to thereby control the level of an
`input signal to the integrated circuit IC. In FIG. 4, reference
`character a represents the level of a desired reception signal.
`A digital AGC method is known as disclosed,
`for
`example,
`in Japanese Patent Laid-open Gazette No.
`10-5 6343. With this method, in accordance with an electric
`field intensity detected from an output of an intermediate
`frequency signal, the gain of a variable gain amplifier is
`controlled, and an output of the variable gain amplifier is
`orthogonally detected, and in accordance with a difference
`between the orthogonally detected IQ output signal ampli-
`tudes and desired IQ output signal amplitudes, the gain of
`the variable gain amplifier is finely adjusted.
`With the conventional
`tuner structure of the satellite
`
`digital radio broadcast receiver described above, it is, how-
`ever, necessary to set a hysteresis to the switching circuit in
`order to prevent the switching between the high frequency
`amplifier 13 and attenuator 14 from being fluttered due to a
`reception signal
`level. A satellite digital radio broadcast
`receiver has as its one objective using it mounted on a
`vehicle. The reception condition during vehicle running is
`influenced by a multi-path and the like so that the signal
`level may change abruptly by 15 dB or more.
`It is therefore necessary that the switching hysteresis is 15
`dB or larger. Further, since a digital modulation method is
`incorporated for the satellite digital radio broadcast, if the
`reception signal is once intercepted, there is some idle time
`before sounds can be reproduced, because data synchroni-
`zation and the like are necessary. A complicated control
`process is therefore required such as matching the switching
`timing for signal level control to the data transition period
`and fixing the synchronization circuit and the like during
`such period.
`the level adjustment of a ground
`From these reasons,
`wave signal input to the integrated circuit IC is something
`intermittent. FIG. 5 shows the disturbance wave elimination
`
`characteristics actually measured. As shown, the character-
`istics are stepwise and there are an input signal level having
`the bad disturbance wave elimination characteristics and an
`
`input signal level having the good disturbance wave elimi-
`nation characteristics. There is a difference of 10 dB or more
`
`between these signal levels. If a signal cannot be received
`once because of the switching hysteresis control, even if the
`disturbance signal level lowers somewhat, it is not so fast
`until the reception is recovered. The hatched area in FIG. 5
`indicates a reception enabled range.
`
`SUMMARY OF THE INVENTION
`
`It is an objective of the present invention to provide a
`satellite digital radio broadcast receiver capable of eliminat-
`ing the above-described disadvantages and improving the
`disturbance wave elimination characteristics with a simple
`structure.
`
`4
`
`According to one aspect of the present invention, there is
`provided a satellite digital radio broadcast receiver having
`an integrated circuit including a first reception series for
`performing a reception processing of a satellite wave signal
`from a satellite and a second reception series for performing
`a reception processing of a ground wave signal from a
`repeater in order to receive both the satellite wave signal and
`the ground wave signal having the same broadcast contents
`and different modulation methods. the satellite digital radio
`broadcast
`receiver comprising: automatic gain control
`means for amplifying a signal from a single antenna at a
`variable gain amplifier, and in accordance with a level of a
`signal outputted from the variable gain amplifier, for c011-
`trolling a gain of the variable gain amplifier to control the
`level of the signal outputted from the variable gain amplifier;
`and a two-way distributor for distributing an output of the
`automatic control means
`to two distribution outputs,
`wherein one distribution output from the two-way distribu-
`tor is supplied to the integrated circuit as an input signal to
`the first reception series, and the other distribution output
`from the two-way distributor is supplied to the integrated
`circuit as an input signal to the second reception series.
`According to the satellite digital radio broadcast receiver,
`the input signals to the first and second reception series of
`the integrated circuit have the levels controlled by the
`automatic gain control means. Therefore, the input signal
`level can be maintained generally constant even if there is a
`sharp change in a disturbance signal level.
`As above, according to the satellite digital radio broadcast
`receiver of this invention, only one series can suffice for the
`input signals to the integrated circuit so that the receiver can
`be made compact and the cost can be reduced.
`
`BRIEF DESCRIPTION OF THE DRAWINGS
`
`FIG. 1 is a diagram showing the outline of a satellite
`digital radio broadcast system.
`FIG. 2 is a diagram showing the spectrum of radio waves
`to be received by a satellite digital radio broadcast receiver.
`FIG. 3 is a block diagram showing the structure of a tuner
`unit of a conventional satellite digital radio broadcast
`receiver.
`
`FIG. 4 is the characteristic diagram explaining the dis-
`turbance signal elimination characteristics of a conventional
`satellite digital radio broadcast receiver.
`FIG. 5 is a schematic diagram explaining a disturbance
`radio wave to be received by a conventional satellite digital
`radio broadcast receiver.
`
`10
`
`15
`
`25
`
`35
`
`40
`
`45
`
`50
`
`FIG. 6 is a block diagram showing the structure of a tuber
`unit of a satellite digital radio broadcast receiver according
`to an embodiment of the invention.
`
`Ln Ln
`
`60
`
`65
`
`FIG. 7 is the characteristic diagram explaining the dis-
`turbance signal elimination characteristics of the satellite
`digital radio broadcast receiver of the embodiment.
`FIG. 8 is a schematic diagram explaining a disturbance
`radio wave to be received by the satellite digital radio
`broadcast receivers of the embodiment and the prior art.
`
`DESCRIPTION OF THE PREFERRED
`EMBODIIVIENT
`
`Description will be made on a satellite digital radio
`broadcast receiver according to an embodiment of the inven-
`tion.
`
`FIG. 6 is a block diagram showing the structure of a tuner
`unit of a satellite digital radio broadcast receiver according
`to the embodiment of the invention.
`
`

`

`US 7,317,894 B2
`
`6
`muting state of an audio signal when the level of an input
`signal to the integrated circuit IC is controlled by the voltage
`control type variable gain amplifier 33 upon reception of the
`disturbance wave a. The high level line indicates the period
`while the muting state is removed and an audio signal is
`obtained, and the low level line indicates the period while
`the muting state is efiected and an audio signal cannot be
`obtained.
`
`As apparent from the comparison between the lines c and
`d in FIG. 8, as compared to the satellite digital radio
`broadcast receiver 20. the satellite digital radio broadcast
`receiver 30 has a shorter sound interception period and a
`shorter reception stop period.
`Since the satellite digital radio broadcast receiver 30 has
`only one series as the front end of the integrated circuit IC,
`it can be made compact and the cost can be reduced.
`As described so far, according to the satellite digital radio
`broadcast receiver, only one series is used as the front end
`of the integrated circuit, and the level of an input signal to
`the integrated circuit is controlled by AGC. Accordingly, the
`satellite digital radio broadcast receiver has a shorter sound
`interception period and a shorter reception stop period.
`Furthermore,
`since the satellite digital
`radio broadcast
`receiver 30 has only one series as the front end of the
`integrated circuit IC, it can be made compact and the cost
`can be reduced.
`
`What is claimed is:
`
`5
`In the satellite digital radio broadcast receiver 30 of the
`embodiment, an antenna 31 receives a satellite wave signal
`and a ground wave signal. The band of the received signal
`is limited by a band-pass filter 32, and an output of the
`band-pass filter 32 is supplied to and amplified at a voltage
`control type variable gain amplifier 33. An output signal
`from the voltage control type variable gain amplifier 33 is
`supplied to a two-way distributor 34 which inputs two-way
`distributed output signals to variable gain amplifiers 15 an
`25 of an integrated circuit IC, respectively. The integrated
`circuit IC has the same structure as the integrated circuit IC
`shown in FIG. 3, and so the description of the structure and
`operation thereof is omitted.
`type variable gain
`An output of the voltage control
`amplifier 33 is detected by a detector 35 to obtain a detection
`voltage corresponding to the input signal level. This detec-
`tion voltage is supplied to a control circuit 36 which converts
`it into anAGC control voltage. The AGC control voltage is
`supplied as a gain control voltage to the voltage control type
`variable gain amplifier 33 to perform AGC and control the
`level of an input signal to the integrated circuit IC. The
`antenna 31 is either an antenna for receiving a satellite wave
`signal or an antenna for receiving a ground wave signal.
`The two-way distributor 34 distributes an input at a
`distribution ratio suitable for gains of two series in the
`integrated circuit IC and supplies the distributed signals to
`the variable gain amplifiers 15 and 25, respectively. Abetter
`one of the demodulation signals of the two series is selected
`and output. similar to conventional techniques.
`As described above, in the tuner unit of the satellite digital
`radio broadcast receiver 30, the level of an input signal to the
`integrated circuit IC is controlled by AGC, and signals
`having AGC controlled levels are distributed to the two
`series of the integrated circuit IC. Therefore, the level of an
`input signal to the integrated circuit IC is controlled con-
`tinuously in an analog fashion, so that the input signal level
`is not switched intermittently as in the case of conventional
`techniques. As indicated at b in FIG. 7, the disturbance
`signal elimination characteristics will not be degraded
`abruptly so that even a sharp change in a disturbance signal
`level can be followed smoothly. In addition, even if the
`receiver is mounted on a vehicle, broadcast reception is
`hardly broken. The disturbance signal elimination charac-
`teristics indicated at a in FIG. 7 are the same as those shown
`in FIG. 5.
`
`FIG. 8 is a schematic diagram showing actual measure-
`ments by the satellite digital radio broadcast receiver 30 of
`the embodiment and the conventional receiver 20, both
`mounted on a vehicle running through the New York city.
`The level of a disturbance wave is indicated at a in FIG. 8.
`A line indicated at b in FIG. 8 shows the selection state
`
`between the high frequency amplifier 13 and attenuator 14.
`The high level line indicates a selection of the high fre-
`quency amplifier 13, and the low level
`line indicates a
`selection of the attenuator 14. A line indicated at c in FIG.
`
`8 schematically illustrates a muting state of an audio output
`when the level of an input signal to the integrated circuit IC
`is controlled by switching between the high frequency
`amplifier 13 and attenuator 14 upon reception of the distur-
`bance wave a. The high level line indicates the period while
`the muting state is removed and an audio signal is obtained,
`and the low level line indicates the period while the muting
`state is elfected and an audio signal cannot be obtained. A
`line indicated at d in FIG. 8 schematically illustrates a
`
`10
`
`15
`
`25
`
`35
`
`40
`
`45
`
`50
`
`Ln Ln
`
`60
`
`1. A satellite digital radio broadcast receiver having an
`integrated circuit including a first reception series for per-
`forming a reception processing of a satellite wave signal
`from a satellite and a second reception series for perfomiing
`a reception processing of a ground wave signal from a
`repeater in order to receive both the satellite wave signal and
`the ground wave signal having the same broadcast contents
`and diiferent modulation methods, a total gain through the
`first reception series being dilferent from a total gain through
`the second reception series. the satellite digital radio broad-
`cast receiver comprising:
`automatic gain control means for amplifying a signal from
`a single antenna at a variable gain amplifier, and in
`accordance with a level of a signal outputted from the
`variable gain amplifier. for controlling a gain of the
`variable gain amplifier to control the level of the signal
`outputted from the variable gain amplifier; and
`a two-way distributor for distributing an output of the
`automatic gain control means to two distribution out-
`puts,
`wherein one of the two distribution outputs from the
`two-way distributor is supplied to said integrated cir-
`cuit as an input signal to the first reception series, and
`the other of the two distribution outputs from the
`two-way distributor is supplied to the integrated circuit
`as an input signal to the second reception series, and
`wherein the two-way distributor operates to distribute an
`input at a distribution ratio according to the dilference
`between the total gain through the first reception series
`and the total gain through the second reception series.
`2. The satellite digital radio broadcast receiver according
`to claim 1, wherein the antenna is either an antenna for
`receiving the satellite wave signal or an antenna for receiv-
`ing the ground wave signal.
`X
`46
`
`if
`
`4%
`
`X
`
`