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    • 1. 发明专利
    • NAVIGATION SYSTEM
    • JPH08221693A
    • 1996-08-30
    • JP2275995
    • 1995-02-10
    • MATSUSHITA ELECTRIC IND CO LTD
    • KAWASAKI AKIHISATATEDA YOSHIFUMI
    • G09B29/00G01C21/00G01S5/02G01S19/14G08G1/0962G08G1/0969
    • PURPOSE: To obtain real-time information concerned in facilities by retrieving the communication number corresponding to the facilities which need information, from a storage device and communicating with the facilities directly through a communication equipment according to the communication number. CONSTITUTION: This system has an arithmetic unit 15 which retrieves the number of communication with the facilities specified by an input device 12, communicates with the facilities through the communication equipment 13 according to the retrieved communication number, and outputs the information obtained by the communication with the facilities through an output device 14. Then, a user specifies the facilities which need information, through the input device 12. The communication number corresponding to the specified facilities is retrieved from the storage device 11, and a communication with the facilities is made through the communication device 13 according to the retrieved communication number to output the information obtained by the communication with the facilities to the output device 14. Therefore, by communicating with the facilities specified on a mobile station side through the communication equipment 13 according to the communication number, the communication with the target facilities becomes possible through easy operation, and information on the facilities can be obtained in real time.
    • 4. 发明专利
    • DIFFUSION SYMBOL CAPTURING CIRCUIT
    • JPH05100007A
    • 1993-04-23
    • JP26445791
    • 1991-10-14
    • MATSUSHITA ELECTRIC IND CO LTD
    • KUWATSURU KEIICHIROIKEDA TAKESHITATEDA YOSHIFUMI
    • G01S19/30G01S19/37
    • PURPOSE:To shorten the time required in capturing in a dispersion symbol capturing circuit, which is used to synchronously capture the dispersion symbol of a GPS satellite electric wave. CONSTITUTION:A shift register 20 emits dispersion symbol signals P1-Pn, which are phase delayed bit by bit. These are entered into a sensing part 30, and the error etc., in the Doppler shift frequency, etc., between the satellite signal and the dispersion symbol signal of the satellite is removed according to the exclusion theory with the signals NI, NQ, etc., given from an NC transmitter 60 and the dispersion symbol signal of the satellite. The remaining signal components are counted by a sampling clock CK, and the correlation result is emitted. A control part judges capture of the dispersion symbol of the satellite signal by searching the maximum among the output data. In case nothing is captured, the search is made while the phase of the dispersion symbol signal PA is shifted in conformity to the control signal given by the control part 70, which is made repetitively until capturing takes place. Thus the dispersion symbol can be captured at a high speed by performing simultaneous searching using sensors in 'n' pieces.
    • 5. 发明专利
    • METHOD FOR MEASURING PSEUDO NOISE CODE OF GPS RECEIVER
    • JPH0420889A
    • 1992-01-24
    • JP12725990
    • 1990-05-16
    • MATSUSHITA ELECTRIC IND CO LTD
    • TATEDA YOSHIFUMIIKEDA TAKESHI
    • G01S1/00G01S19/29G01S19/30
    • PURPOSE:To obtain the highly accurate measured value of the phase of a pseudo noise code without tracking and drawing the pseudo noises by obtaining the change in phase of the pseudo noise code based on the change in phase of a carrier wave, and performing subtraction between the phase errors of the estimated value of the pseudo noise code and the received signal. CONSTITUTION:In a demodulator part 9 of a GPS receiver, the phase errors of a pseudo noise code and a carrier wave are independently measured. The measured results are delivered into a control part 8. When the radio wave from a satellite is interrupted, a pseudo-noise-code generating part 10 is controlled, and the pseudo noise code is scanned. Then the satellite signal is detected with the demodulator part 9. The phase of the pseudo noise code when the signal is detected at the next time is set in the generator 10. The phase of the pseudo noise code is measured with the demodulator part 9. Thereafter, whether the signal of the satellite is received or not is confirmed. Then, the phase of the pseudo noise code is changed. Then, the phase of the pseudo noise code of the satellite signal is computed by the operation based on the preset value and the changed value of the pseudo noise code and the frequency of the regenerated carrier wave. The value is outputted as the measured value.