JP5695839B2 - Receiver - Google Patents

Description

  The present invention relates to a receiving technique, and relates to a receiving apparatus that receives a signal transmitted from a satellite.

  GPS (Global Positioning System) is used for “real-time GPS” that immediately acquires position information. GPS is also used for GeoTagging. Geotagging is a technique for embedding position information by tags in a digital camera or camera-equipped mobile phone. For example, when a user takes a picture, the location where the picture was taken is recorded by geotagging. In general, even for geotagging, position information is measured in real time. It should be noted that the acquisition of the position information requires a time from 30 seconds to a maximum of several minutes. The longer the time for acquisition, the worse the usability for the user and the more the power consumption.

  In order to cope with this, in the technique disclosed in Non-Patent Document 1, when a user takes a picture with a digital camera, information is acquired by a GPS receiver in the same manner as real-time GPS. However, at this time, only the PRN number of the GPS satellite and the pseudo distance information from the GPS satellite to the digital camera are acquired. These information, photo data, and shooting time information are associated with each other and stored in the digital camera as basic data. When the user comes home, the client side software on the personal computer (PC) is used to obtain basic data stored in the digital camera. Then, the server side software service is accessed via the Internet. At that time, detailed information of each GPS satellite at each time is downloaded. The detailed information and basic data are used, and the client-side software on the personal computer calculates the position information.

Takeshi Enomoto, “Location information is enough if you know later”, [online], September 3, 2009, EDN JAPAN, [Search March 17, 2010], Internet <URL: http: //ednjapan.rbi -j.com/news/2009/9/5472>

  With the above-described technique, the position information is not known at the time of shooting, and the position information can be found later by calculation on a PC or a server. For this reason, at the time of shooting, it is unclear whether the accuracy of the data used to calculate position information later is high or low. Therefore, data stored in the digital camera at the time of shooting may be wasted. For example, the accuracy of collected data tends to be low in shooting in an environment where the line-of-sight direction of the signal from each GPS satellite is blocked. However, since the elevation angle and azimuth angle of each GPS satellite are unknown to the user, it is difficult to determine whether or not usable data has been collected.

  The present invention has been made in view of such circumstances, and an object thereof is to provide a technique for quickly estimating the accuracy of a signal received from a satellite.

  In order to solve the above problems, a receiving device according to an aspect of the present invention includes a receiving unit that receives a signal transmitted from at least one satellite, and a local signal for frequency-converting the signal received by the receiving unit. And generating a local signal whose frequency changes over a range of Doppler shift that can occur in the signal received in the receiving unit, and frequency-converting the signal received in the receiving unit by the local signal generated in the generating unit A conversion unit, a detection unit for detecting an envelope of the frequency-converted signal in the conversion unit, a comparison unit for comparing the signal detected by the envelope in the detection unit with a threshold value, and a comparison result as a result of the comparison unit. Transmitting the signal received at the receiver by counting the number of signal components And a estimation unit that estimates the number of satellites to be.

  According to this aspect, in the signal frequency-converted with the local signal whose frequency changes over the range of Doppler shift that can occur in the received signal, the number of signal components that are equal to or greater than the threshold value is counted. The number of satellites can be estimated early.

  You may further provide the memory | storage part which memorize | stores the signal received in the receiving part. The conversion unit may read the signal stored in the storage unit a plurality of times and frequency-convert the read signal. In this case, since the stored signal is read out a plurality of times, the processing period can be shortened.

  The generation unit includes a plurality of partial generation units, and when the range of Doppler shift that can be generated in the signal received by the reception unit is divided into a plurality of partial ranges, each partial generation unit has a frequency over a different partial range. The conversion unit includes as many partial conversion units as the number of partial generation units, and each partial conversion unit is generated by a local signal generated in a different partial generation unit. The signal received by the reception unit may be frequency converted, and the detection unit may output an envelope detection result of a signal obtained by combining the signals subjected to frequency conversion in each of the plurality of partial conversion units. In this case, since the frequency conversion process is performed in parallel, the processing period can be shortened.

  Another embodiment of the present invention is also a receiving device. The apparatus includes a receiving unit that receives a signal transmitted from at least one satellite, a conversion unit that converts a signal received in the receiving unit from a time domain signal to a frequency domain signal, and a conversion unit. The comparison unit that compares the frequency domain signal converted in the unit with a threshold value and the reception unit receives the signal by counting the number of signal components that are equal to or greater than the threshold value as a result of the comparison in the comparison unit And an estimation unit for estimating the number of satellites from which the signal is transmitted.

  According to this aspect, since the number of signal components having a value equal to or greater than the threshold value is counted in the frequency domain signal subjected to Fourier transform, the number of satellites can be estimated at an early stage.

  You may further provide the notification part which notifies the number of the satellites estimated in the estimation part. In this case, the user can be notified of the number of satellites.

  It should be noted that any combination of the above-described constituent elements and a conversion of the expression of the present invention between a method, an apparatus, a system, a recording medium, a computer program, etc. are also effective as an aspect of the present invention.

  According to the present invention, the accuracy of a signal received from a satellite can be estimated at an early stage.

It is a figure which shows the structure of the receiver which concerns on the Example of this invention. It is a figure which shows the structure of the multiplication part of FIG. It is a figure which shows the structure of the frequency discrimination part of FIG. 4A to 4D are diagrams illustrating waveforms of signals generated in the frequency discriminating unit in FIG. It is a figure which shows the structure of the frequency discrimination part which concerns on the modification of this invention. It is a figure which shows the structure of the receiver which concerns on another modification of this invention.

  Before describing the present invention specifically, an outline will be given first. An embodiment of the present invention relates to a GPS receiver that receives a signal from a GPS satellite and measures position information. In particular, the receiving apparatus A / D converts the received signal and then stores the signal for a predetermined period. Thereafter, a device equipped with a PC or a GPS calculator measures the position information by executing a position calculation based on a signal stored in the receiving device. As a premise of the present invention, a GPS receiver is mounted on the digital camera. The purpose is to use the photo taken by the user for file management of the shooting location and collation with a map. However, as described above, when positioning position information in real time, a positioning period of at least about 30 seconds is required. For this reason, there is an inconvenience of holding the digital camera at that location for a long time in order to measure the position information even if the photo is taken for a moment. In addition, since the amount of processing for positioning position information is large, power consumption increases and battery life is shortened.

  On the other hand, apart from calculating the position information in real time, at the time of shooting, only signals received from GPS satellites are collected as data. In this case, after the photographing is completed, the PC acquires orbit data of GPS satellites from a predetermined server using the Internet line. Further, the PC obtains position information by calculation based on the trajectory data and the collected data. In this case, since data can be collected once in about 200 msec, convenience for the user is improved and power consumption is reduced. However, it cannot be determined at the time of shooting whether the data collected by the user can be used to derive position information. Here, the case where the data cannot be used for deriving the position information means that the accuracy of the position information also deteriorates because the data accuracy deteriorates due to a small number of GPS satellites as transmission sources. It is. In order to cope with this, the receiving apparatus according to the present embodiment executes the following processing.

  When receiving signals from a plurality of GPS satellites, the receiving apparatus according to the present embodiment utilizes the fact that the amount of Doppler shift differs for each GPS satellite, and stores the data in the memory. Is used to estimate the quality of the data. That is, since the frequency of the signal from each of the plurality of GPS satellites is different due to the Doppler shift, the number of GPS satellites that are transmission sources is estimated by counting the number of signals in the frequency domain. Further, when the estimated number of GPS satellites is three or more, the receiving apparatus notifies that the data quality is high by turning on the LED for a certain period of time. On the other hand, when the estimated number of GPS satellites is less than 3, the receiving device lights up another LED for a certain period of time.

  FIG. 1 shows a configuration of a receiving apparatus 100 according to an embodiment of the present invention. The receiving apparatus 100 includes an antenna 10, an RF amplification unit 12, a mixer 14, an IF amplification unit 16, an A / D conversion unit 18, a CPU 20, a reference oscillation unit 22, a local oscillation unit 24, a multiplication unit 26, a frequency discrimination unit 28, and a switch. Unit 30, an interface unit 32, a flash memory 34, and an LED display unit 36. The switch unit 30 receives an activation instruction from the user. When an activation instruction is received, power from a battery (not shown) is supplied to the entire receiving apparatus 100. Here, it is assumed that the receiving apparatus 100 is provided in a digital camera (not shown). Hereinafter, processing of the receiving apparatus 100 when an imaging function is executed in the digital camera (not shown) will be described.

  The antenna 10 receives an RF signal transmitted from a GPS satellite (not shown) and transmitted from at least one GPS satellite. In addition, instead of GPS, Galileo (Galileo positioning system) and GLONASS (Global Navigation Satellite System) may be used. The antenna 10 outputs the received RF signal to the RF amplification unit 12. The RF amplifier 12 amplifies the RF signal input from the antenna 10. The RF amplification unit 12 outputs the amplified RF signal to the mixer 14.

  The reference oscillation unit 22 is a crystal oscillator and outputs, for example, a 16.368 MHz signal to the local oscillation unit 24. The local oscillating unit 24 outputs a signal synchronized with the signal from the reference oscillating unit 22, for example, a signal of 1571.328 MHz, which is 96 times the frequency, to the mixer 14. The mixer 14 receives the RF signal from the RF amplification unit 12 and also receives the signal from the local oscillation unit 24. The mixer 14 converts the RF signal into an IF signal based on the signal from the local oscillation unit 24. The frequency of the IF signal is, for example, 4.092 MHz. The mixer 14 outputs the IF signal to the IF amplification unit 16. The IF amplifying unit 16 amplifies the IF signal from the mixer 14. The IF amplifier 16 outputs the IF signal to the A / D converter 18. The A / D converter 18 generates a digital signal by performing analog / digital conversion on the IF signal from the IF amplifier 16. The A / D converter 18 outputs the digital signal to the CPU 20 and the multiplier 26.

  The CPU 20 executes various processes in the receiving device 100. One of various processes is a storage process. The CPU 20 samples the digital signal from the A / D converter 18 over a period of about 200 ms and stores the digital signal of about 1 Mbit in the flash memory 34. At that time, the CPU 20 also stores time data and an ID number measured by a crystal oscillator for a clock of an RTC transmitter (not shown) in the flash memory 34 together with a digital signal.

  The flash memory 34 stores digital signals and the like in accordance with instructions from the CPU 20. The data stored in the flash memory 34 includes C / A codes and carrier signals for each GPS satellite. The flash memory 34 may be a memory of a format that can be detached from the receiving device 100. When calculating position information on the PC after shooting, the CPU 20 supplies the data stored in the flash memory 34 to the PC via the interface unit 32.

  The multiplier 26 receives the digital signal from the A / D converter 18. The multiplication unit 26 performs a multiplication process on the digital signal. Here, the multiplication processing in the multiplication unit 26 will be described with reference to FIG. FIG. 2 shows the configuration of the multiplication unit 26. The multiplication unit 26 includes a delay unit 40 and an EX-OR circuit 42. One of the outputs from the A / D conversion unit 18 (not shown) is input to the delay unit 40. Since the frequency of the digital signal is 4.092 MHz, the period is about 240 nsec. The delay unit 40 delays about 60 nsec of a quarter cycle of the digital signal using a resistor and a capacitor. The EX-OR circuit 42 receives a digital signal from the A / D converter 18 (not shown) and a digital signal from the delay unit 40. The EX-OR circuit 42 generates a doubled 8.184 MHz digital signal (hereinafter also simply referred to as “digital signal”).

The digital signal before being doubled is subjected to BPSK by a spread signal of a C / A code unique to a GPS satellite. In the digital signal multiplied by 2, the C / A code of each GPS satellite is canceled and only the carrier component remains. As a result, the influence of the Doppler shift due to the relative Doppler effect between each GPS satellite and the receiving device 100 remains. For this reason, the carrier frequency of the RF signal from each GPS satellite is shifted within a range of about ± 5 kHz due to Doppler shift. With a digital signal multiplied by 2, the Doppler shift of each GPS satellite is also doubled and can be shifted within a range of about ± 10 kHz. This corresponds to a frequency shift of 8.174 to 8.194 MHz. On the other hand, the deviation due to the frequency accuracy of the reference oscillation unit 22 is added to the above frequency deviation. When the frequency accuracy of the reference oscillating unit 22 is ± 0.5 ppm, the digital signal before the multiplication by 2 is (16.368 × 10 ⁶ ) × 96 × (± 0.5 × 10 ⁻⁶ ) = ± 785.664 Hz. The frequency is shifted. As a result, although the frequency shift is about ± 1.57 kHz in the doubled digital signal, this frequency shift is small with respect to the influence of the Doppler shift. Therefore, the frequency shift is ignored below. Returning to FIG.

  The frequency discriminating unit 28 inputs the digital signal from the multiplication unit 26. The frequency discriminating unit 28 estimates the number of GPS satellites that are transmission sources of signals included in the digital signal. Here, the estimation process in the frequency discriminating unit 28 will be described with reference to FIG. FIG. 3 shows the configuration of the frequency discriminating unit 28. The frequency discriminator 28 includes a mixer 50, a BPF 52, a detector 54, a comparator 56, a sawtooth generator 58, and a VCO oscillator 60.

  The sawtooth wave generator 58 receives a trigger signal having a fixed period T from the CPU 20 and generates a sawtooth wave synchronized with the trigger signal. Here, FIGS. 4A to 4D are used to describe the signals generated in the frequency discriminating unit 28. FIG. 4A to 4D show waveforms of signals generated in the frequency discriminating unit 28. FIG. FIG. 4A shows a trigger signal from the CPU 20. The trigger signal includes a plurality of pulse signals, and the interval between adjacent pulse signals is T. FIG. 4B shows a sawtooth wave generated in the frequency discriminating unit 28. The value changes from L to H at a constant slope from the timing of a predetermined pulse signal in the trigger signal to the timing of the next pulse signal. Further, the value changes from H to L at the timing of the pulse signal. Here, it is assumed that H> L. The description of FIGS. 4C to 4D will be described later. Returning to FIG.

  The VCO oscillator 60 receives the sawtooth wave from the sawtooth wave generator 58. The VCO oscillating unit 60 outputs a local signal whose frequency changes according to the sawtooth wave. Here, the frequency of the local signal output from the VCO oscillating unit 60 varies, for example, between 8.164 and 8.184 MHz. Here, the changing frequency width of 20 kHz is the maximum value of the Doppler shift that can occur between the GPS satellite and the receiving apparatus 100. That is, the VCO oscillating unit 60 is a local signal for frequency-converting the digital signal from the multiplying unit 26, and a local signal whose frequency changes over a range of Doppler shift that can be generated in an RF signal from a GPS satellite. Occur.

  The mixer 50 receives the local signal from the VCO oscillation unit 60 and the digital signal from the multiplication unit 26. The mixer 50 frequency-converts the digital signal with the local signal (hereinafter, the frequency-converted digital signal is also referred to as “digital signal”). The value of the digital signal increases at a frequency corresponding to the signal component included in the digital signal within the frequency range that the local signal can take. The mixer 50 outputs a digital signal to the BPF 52.

  The BPF 52 receives the digital signal from the mixer 50 and extracts a low frequency component. The BPF 52 outputs a digital signal (hereinafter referred to as “digital signal”) obtained by extracting the low frequency component to the detection unit 54. The detector 54 receives a digital signal from the BPF 52. The detector 54 performs envelope detection on the digital signal. Assuming that the BPF 52 has a center frequency of 10 kHz and a bandwidth of 300 Hz, the digital signal (hereinafter referred to as “digital signal”) detected by the envelope in the detector 54 has a frequency in which the Doppler frequency of each GPS satellite is in the range of 10 to 30 kHz. Has been converted. FIG. 4C shows a digital signal subjected to envelope detection in the detection unit 54. A, b, c, d, e, and f shown in FIG. 4C are Doppler frequencies of the respective GPS satellites. The other waveforms correspond to background noise. Returning to FIG. The detector 54 outputs a digital signal to the comparator 56.

  The comparison unit 56 receives the digital signal from the detection unit 54. The comparison unit 56 compares the digital signal with a threshold value. FIG. 4C also shows a threshold value, and the comparison unit 56 extracts a signal component that is equal to or higher than the threshold value, and deletes other signal components. In FIG. 4C, signal components corresponding to c and e having weak received power are deleted. Here, the threshold value is set to, for example, a value corresponding to −140 dBm. -140 dBm is the received power necessary for the calculation for deriving the position information in the PC. FIG. 4D shows a comparison result in the comparison unit 56. The waveform in FIG. 4D is obtained, and four signal components a, b, d, and f are selected. Returning to FIG.

  The CPU 20 receives the comparison result from the comparison unit 56. The CPU 20 estimates the number of GPS satellites that are RF signal transmission sources by counting the number of signal components included in the comparison result, that is, the number of signal components that are equal to or greater than the threshold value. In general, if the number of GPS satellites is three or more, positioning of position information becomes possible. Therefore, if the number of GPS satellites is three or more, the CPU 20 lights the LED display unit 36 in a predetermined color, for example, green. On the other hand, if the number of GPS satellites is less than 3, the CPU 20 lights the LED display unit 36 in another color, for example, red. If the number of GPS satellites is 3 or more, the LED display unit 36 may be lit, and if the number of GPS satellites is less than 3, the LED display unit 36 may blink. In this manner, the LED display unit 36 notifies the number of GPS satellites estimated by the CPU 20.

  This configuration can be realized in terms of hardware by a CPU, memory, or other LSI of any computer, and in terms of software, it can be realized by a program loaded in the memory, but here it is realized by their cooperation. Draw functional blocks. Accordingly, those skilled in the art will understand that these functional blocks can be realized in various forms by hardware only, software only, or a combination thereof.

  Next, a modified example of the present invention will be described. Similar to the embodiment, the modified example relates to a receiving apparatus that estimates the number of GPS satellites that are the transmission source of received RF signals. In the frequency discriminating unit in the receiving apparatus according to the embodiment, one VCO oscillating unit and one mixer are provided. However, in the frequency discriminating unit in the receiving apparatus according to the modification, a plurality of VCO oscillating units are provided in parallel, and a plurality of mixers 50 are also provided so as to correspond to each VCO oscillating unit on a one-to-one basis. . The receiving apparatus 100 according to the modification is the same type as that in FIG. Here, the difference will be mainly described.

  FIG. 5 shows the configuration of the frequency discriminating unit 28 according to a modification of the present invention. The frequency discriminator 28 includes a first mixer 50a, a second mixer 50b, a third mixer 50c, a fourth mixer 50d, and a first BPF 52a, a second BPF 52b, a third BPF 52c, a fourth BPF 52d, First detection unit 54a, second detection unit 54b, third detection unit 54c, fourth detection unit 54d, collectively referred to as unit 54, first comparison unit 56a, second comparison unit 56b, generally referred to as comparison unit 56, A third comparison unit 56c, a fourth comparison unit 56d, a synthesis unit 70, a sawtooth wave generation unit 58, a VCO oscillation unit 60, a first VCO oscillation unit 60a, a second VCO oscillation unit 60b, a third VCO oscillation unit 60c, and a fourth VCO. The oscillator 60d is included.

  The first VCO oscillating unit 60a to the fourth VCO oscillating unit 60d generate local signals whose frequencies change over different ranges. Here, it is assumed that the range of Doppler shift that can occur in the RF signal is divided into a plurality of partial ranges, for example, four partial ranges. As described above, since the range of the Doppler shift that can occur in the RF signal is 20 kHz, each partial range is 5 kHz. For this reason, the frequency of the local signal output from each VCO oscillating unit 60 changes over different partial ranges of 5 kHz.

  The first mixer 50a to the fourth mixer 50d are provided in a one-to-one correspondence with the first VCO oscillating unit 60a to the fourth VCO oscillating unit 60d. Therefore, the number of mixers 50 and the number of VCO oscillating units 60 are the same. Each mixer 50 frequency-converts a digital signal using local signals generated in different VCO oscillating units 60. That is, each mixer 50 performs frequency conversion in parallel. The first BPF 52a to the fourth BPF 52d are provided to have a one-to-one correspondence with the first mixer 50a to the fourth mixer 50d, and the first detection unit 54a to the fourth detection unit 54d have a one-to-one correspondence with the first BPF 52a to the fourth BPF 52d. It is provided to correspond. The first detection unit 54 a to the fourth detection unit 54 d perform envelope detection on the digital signal frequency-converted in each of the plurality of mixers 50. The synthesizer 70 synthesizes the envelope detection results from the first detector 54a to the fourth detector 54d. The synthesizer 70 outputs an envelope detection result of the combined digital signal. Note that the detection unit 54 may be provided in the subsequent stage of the synthesis unit 70.

  Next, another modification of the present invention will be described. Another modification relates to a receiving apparatus that estimates the number of GPS satellites that are the transmission sources of received RF signals, as in the embodiment. In the receiving apparatus according to the embodiment, a frequency discriminating unit is used. On the other hand, a receiving apparatus according to another modification uses FFT instead of the frequency discriminating unit. A receiving apparatus 100 according to another modification is the same type as that in FIG. Here, the difference will be mainly described.

  FIG. 6 shows a configuration of a receiving apparatus 100 according to another modification of the present invention. In FIG. 6, only the configuration from the multiplication unit 26 to the CPU 20 in the reception device 100 is shown. In FIG. 1, the frequency discriminating unit 28 is provided between the multiplication unit 26 and the CPU 20, but in FIG. 6, the fixed oscillation unit 80, the mixer 82, and the LPF 84 are provided therebetween. The multiplier 26 outputs a digital signal multiplied by 2 as before. The frequency of the digital signal is 8.184 MHz. On the other hand, the fixed oscillation unit 80 outputs a local signal having a fixed frequency. The frequency of the local signal is set to 8.174 MHz.

  The mixer 82 receives the digital signal from the multiplication unit 26 and also receives the local signal from the fixed oscillation unit 80. The mixer 82 frequency-converts the digital signal with the local signal. The mixer 82 outputs a frequency-converted digital signal (hereinafter referred to as “digital signal”) to the LPF 84. As a result, a digital signal having a range of 8.174 to 8.194 MHz before frequency conversion becomes a digital signal having a range of 0 to 20 kHz after frequency conversion. The LPF 84 extracts a low frequency component of the digital signal. The LPF 84 outputs a digital signal (hereinafter referred to as “digital signal”) obtained by extracting the low frequency component to the CPU 20.

  The CPU 20 receives the digital signal from the LPF 84 and performs a Fourier transform on the digital signal, thereby converting the signal in the time domain to the signal in the frequency domain. The CPU 20 performs the same processing as the comparison unit 56 on the frequency domain signal. Further, the CPU 20 estimates the number of GPS satellites that are RF signal transmission sources by counting the number of signal components that are equal to or greater than the threshold value as a result of the comparison.

  According to the embodiment of the present invention, the number of signal components having a value equal to or greater than a threshold value is counted in a signal frequency-converted by a local signal whose frequency changes over a range of Doppler shift that can occur in an RF signal. Therefore, the number of GPS satellites that can be used for the calculation for deriving the position information can be estimated at an early stage. Further, since the number of GPS satellites is estimated early, the number of GPS satellites can be notified to the user early. Moreover, since the number of GPS satellites is notified to the user at an early stage, the convenience for the user can be improved. Further, since the number of GPS satellites is estimated early, power consumption can be reduced. In addition, since the frequency conversion process is executed in parallel, the processing period can be shortened. In addition, since the number of signal components having a value equal to or greater than the threshold value in the frequency domain signal subjected to Fourier transform is counted, the number of GPS satellites can be estimated at an early stage.

  In addition, it is possible to determine whether or not the data received from the GPS satellite is acceptable at the time of photographing before connection with the PC, and even if the data acquired by the user is negative, the data can be collected again. Further, since the data can be collected again, the data can be collected with peace of mind for the user. Further, since unnecessary data is not saved, the amount of effective data collected can be increased under the limitation of ROM capacity. Further, since the sample data is sampled during data storage of about 200 msec, power consumption can be reduced. Further, when the receiving device is incorporated in a digital camera, the CPU is shared, so that the circuit can be simplified, and downsizing and cost reduction can be realized.

  In the above, this invention was demonstrated based on the Example. This embodiment is an exemplification, and it will be understood by those skilled in the art that various modifications can be made to combinations of the respective constituent elements, and such modifications are also within the scope of the present invention.

  In the embodiment of the present invention, the multiplier 26 receives the digital signal from the A / D converter 18, and the frequency discriminator 28 receives the digital signal from the multiplier 26. However, the present invention is not limited to this. For example, the digital signal from the A / D converter 18 may be stored in the flash memory 34 without being output to the multiplier 26. The digital signal stored in the flash memory 34 may be output to the multiplication unit 26 and the frequency discrimination unit 28. At that time, the digital signal may be read from the flash memory 34 a plurality of times. The mixer 50 of the frequency discriminating unit 28 converts the frequency of the digital signal read a plurality of times. Here, since the period T in FIG. 4A is set to about 1 sec, the operation of the receiving apparatus 100 requires about 1 sec. For example, when the digital signal stored in the flash memory 34 is read five times, the operation of the receiving device 100 is shortened to about 200 msec. According to this modification, user convenience can be further improved. Moreover, power consumption can be further reduced.

  In the embodiment of the present invention, the CPU 20 notifies the number of GPS satellites via the LED display unit 36. However, the present invention is not limited to this. For example, the CPU 20 may output a buzzer sound through a speaker (not shown). At that time, the tone of the buzzer may be changed according to the number of GPS satellites. In addition, a sound may be output instead of the buzzer sound. Further, a display may be provided, and the CPU 20 may display the number of GPS satellites on the display. According to this modification, the number of GPS satellites can be notified in various forms.

  10 antennas, 12 RF amplification units, 14 mixers, 16 IF amplification units, 18 A / D conversion units, 20 CPUs, 22 reference oscillation units, 24 local oscillation units, 26 multiplication units, 28 frequency discrimination units, 30 switch units, 32 Interface unit, 34 flash memory, 36 LED display unit, 40 delay unit, 42 EX-OR circuit, 50 mixer, 52 BPF, 54 detection unit, 56 comparison unit, 58 sawtooth wave generation unit, 60 VCO oscillation unit, 100 reception apparatus.

Claims (2)

A receiver for receiving a signal transmitted from at least one satellite;
The frequency is a local signal for frequency-converting the signal received by the receiving unit, and the frequency is in accordance with a sawtooth wave synchronized with a certain period over a range of Doppler shift that can occur in the signal received by the receiving unit. A generator for generating a changing local signal;
A conversion unit that converts the frequency of a signal received at the reception unit by a local signal generated at the generation unit;
A detector for detecting an envelope of the frequency-converted signal in the converter;
A comparison unit that compares the envelope-detected signal with a threshold value in the detection unit;
The comparison in the comparison unit result, by counting the number of signal components that are equal to or greater than a value threshold, and a estimation unit that estimates the number of satellites from which it receives the signal received at the receiving unit Prepared,
The generation unit includes a plurality of partial generation units, and when the range of Doppler shift that can be generated in the signal received by the reception unit is divided into a plurality of partial ranges, each partial generation unit has different partial ranges. A local signal whose frequency changes over time,
The conversion unit includes the same number of partial conversion units as the number of partial generation units, and each partial conversion unit uses a local signal generated in a different partial generation unit to generate a frequency of a signal received in the reception unit. Converted,
The detection unit outputs an envelope detection result of a signal obtained by combining signals obtained by frequency conversion in each of a plurality of partial conversion units. The receiving device according to claim 1, further comprising a notification unit that notifies the number of satellites estimated by the estimation unit.

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