Diversity type global positioning system for motor vehicles

• US 5,341,301 A
• Filed: 12/23/1991
• Issued: 08/23/1994
• Est. Priority Date: 12/27/1990
• Status: Expired due to Term

• Current Assignee: Nippondenso Co., Ltd. (DENSO Corporation)
• Original Assignee: Nippondenso Co., Ltd. (DENSO Corporation)
• Inventors: Ozaki, Yoshitaka, Shirai, Kazunari, Fukaya, Hiroyasu
• Primary Examiner(s): Black, Thomas G.
• Assistant Examiner(s): ZANELLI, MICHAEL J
• Application Number:
  US07/812,102
• Time in Patent Office: 974 Days
• Field of Search: 364/449, 364/452, 342/457, 342/464, 342/357
• US Class Current: 701/215
• CPC Class Codes: G01S 19/14 specially adapted for specific applications
• CPC Class Codes: G01S 19/24 Acquisition or tracking or demodulation of signals transmitted by the system synchronisation aspects of direct sequence spread spectrum modulation H04B1/7073
• CPC Class Codes: G01S 19/35 Constructional details or hardware or software details of the signal processing chain
• CPC Class Codes: G01S 19/42 Determining position
• CPC Class Codes: H04B 7/082 selecting best antenna path

Abstract

This diversity type GPS system for a vehicle has first and second antennas mounted at first and second locations, respectively, inside a vehicle. First and second high frequency amplifiers and an antenna changer apply the signals received by the first and second antennas to first and second SS demodulators. The first and second SS demodulators simultaneously perform search operations for satellites, and demodulate rf signals (demodulated data) from the searched out satellites. An arithmetic and control unit computes a position of the vehicle from the demodulated data once three or more sets of demodulated data are available. The arithmetic and control unit also controls the antenna changer to switch the antenna from which a demodulator receives signals so as to improve the searching operations of the demodulators.

Claims

1. A diversity type GPS for a vehicle for computing a position of the vehicle on the basis of rf signals received from a plurality of satellites, comprising:

first and second antennas, mounted at first and second discrete positions, respectively, in a compartment of a vehicle, for receiving rf signals from a plurality of satellites, and

signal receiving means for demodulating rf signals from said satellites on the basis of signals received from said first and second antennas, and for computing a position of said vehicle on the basis of the demodulated data,

said signal receiving means comprising;

first and second demodulators, each for receiving a search command for a specific satellite, for performing a satellite search operation in accordance with said signals received by a selected one of said first and second antennas, and for demodulating said received signals when said satellite search operation is effected,

first switching means for selectively inputting signals received from said first and second antennas to said first demodulator,

second switching means for selectively inputting signals received from said first and second antennas to said second demodulator,

control means for outputting said search command for a first satellite to said first demodulator, for outputting a first antenna selection command for selection of either said first or second antenna to said first switching means, for outputting said search command for a second satellite to said second demodulator, and for outputting a second antenna selection command for selection of either said first or second antenna to said second switching means, and

computing means for computingthe position of said vehicle, wherein

said first and second demodulators simultaneously search out said first and second satellites.

2. A diversity type GPS according to claim 1, wherein said control means comprises means for controlling said first and second switching means respectively, during said respective search operation of said first and second demodulators, so as to switch from a selected one of said first and second antennas to the other one of said first and second antennas after a first predetermined time, and means for continuing said search operation for a second predetermined time by using signals received from said other one of said first and second antenna thus switched, and wherein said control means outputs said search command for a third satellite to said first demodulator as soon as said first satellite is found by said first demodulator while said second demodulator continues to search out said second satellite.

5. A diversity type GPS according to claim 1, wherein said control means further comprises means for successively repeating the search operation by said first and second demodulators between a larger number of selected satellites than the number of said first and second satellites.

6. A diversity type GPS according to claim 1, wherein said first and second switching means comprises analog switches respectively.

7. A diversity type GPS according to claim 1, further comprising high-frequency amplifying means for amplifying signals received by said first and second antennas and applying the amplified signals to said first and second switching means.

8. A diversity type GPS according to claim 1, further comprising a third demodulator mounted in parallel with said first and second demodulators, and third switching means for inputting, into said third demodulator, signals received from said first and second antennas.

3. A diversity type GPS for a vehicle for computing a position of the vehicle on the basis of rf signals received from a plurality of satellites, comprising:

first and second antennas, mounted at first and second discrete positions, respectively, in a compartment of a vehicle for receiving rf signals from a plurality of satellites, and

signal receiving means for demodulating rf signals from said satellites on the basis of signals received from said first and second antennas, and for computing a position of said vehicle on the basis of the demodulated data,

said signal receiving means comprising;

first and second demodulators, each for receiving a search command for a specific satellite, for performing a satellite search operation in accordance with said signals received by a selected one of said first and second antennas, and for demodulating said received signals when said satellite search operation is effected,

first switching means for selectively inputting signals received from said first and second antennas to said first demodulator,

second switching means for selectively inputting signals received from said first and second antennas to said second demodulator,

control means for outputting said search command for a first satellite to said first demodulator, for outputting a first antenna selection command for selection of either said first or second antenna to said first switching means, for outputting said search command for a second satellite to said second demodulator, and for outputting a second antenna selection command for selection of either said first or second antenna to said second switching means, and

computing means for computing the position of said vehicle, wherein

said first and second demodulators simultaneously search out said first and second satellites,

said control means comprises means for controlling said first and second switching means respectively, during said respective search operation of said first and second demodulators, so as to switch from a selected one of said first and second antennas to the other one of said first and second antennas after a first predetermined time, and means for continuing said search operation for a second predetermined time by using signals received from said other one of said first and second antenna thus switched, and

said control means further comprises means for changing the switching timing of said first and second antennas in order to improve the rate of use of the one of said first and second antenna which was effective in a previous search operation when searching out the same satellite.

4. A diversity type GPS for a vehicle for computing a position of the vehicle on the basis of rf signals received from a plurality of satellites, comprising:

first and second antennas, mounted at first and second discrete positions, respectively, in a compartment of a vehicle for receiving rf signals from a plurality of satellites, and

signal receiving means for demodulating rf signals from said satellites on the basis of signals received from second antennas, and for computing a position of said vehicle on the basis of the demodulated data,

said signal receiving means comprising;

first and second demodulators, each for receiving a search command for a specific satellite, for performing a satellite search operation in accordance with said signals received by a selected one of said first and second antennas, and for demodulating said received signals when said satellite search operation is effected,

first switching means for selectively inputting signals received from said first and second antennas to said first demodulator,

second switching means for selectively inputting signals received from said first and second antennas to said second demodulator,

control means for outputting said search command for a first satellite to said first demodulator, for outputting a first selection command for selection of either said first or second antenna to said first switching means, for outputting said search command for a second satellite to said second demodulator, and for outputting a second antenna selection command for selection of either said first or second antenna to said second switching means,

computing means for computing the position of said vehicle, and

a terrestrial magnetism sensor for sensing the vehicle'"'"'s direction of travel, and wherein

said first and second demodulators simultaneously search out said first and second satellites,

said control means comprises means for controlling said first and second switching means respectively, during said respective search operation of said first and second demodulators, so as to switch from a selected one of said first and second antennas to the other one of said first and second antennas after a first predetermined time, and means for continuing said search operation for a second predetermined time by using signals received from said other one of said first and second antenna thus switched, and

said control means further comprises means for storing data of the rate of use of said first and second antennas on the basis of relative azimuths of said satellites relative to the direction of said vehicle, means for detecting said relative azimuth of said specific satellite, and means for changing the switching timing of said first and second antennas on the basis of said detected relative azimuth.

9. A diversity type GPS for a vehicle for computing a position of the vehicle on the basis of rf signals received from a plurality of satellites, comprising:

first and second antennas, mounted at first and second discrete positions, respectively, in a compartment of a vehicle, for receiving rf signals from a plurality of satellites, and

signals receiving means for demodulating rf signals from said satellites on the basis of signals received from said first and second antennas and for computing a position of said vehicle on the basis of the demodulated data,

said signal receiving means comprising;

first and second demodulators, each for receiving a search command for a specific satellite, for performing a satellite search operation in accordance with said signals received by a selected one of said first and second antennas, and for demodulating said received signals when said search operation is effected,

switching means for selectively inputting signals received from said first and second antennas to said first and second demodulators,

control means for simultaneously outputting said search command for a first satellite to said first demodulator and said search command for a second satellite to said second demodulator, and for outputting said search command for a third satellite to said first demodulator as soon as said search operation for said first satellite is effected, even if the search operation of said second satellite by said second demodulator continues, and

computing means for computing the position of said vehicle.

10. A diversity type GPS according to claim 9, wherein said control means controls said switching means so that, during the search operation for said first satellite by said first demodulator, one of said first and second antennas which is connected to said demodulator is switched to the other one of said first and second antennas.

11. A diversity type GPS according to claim 10, wherein said control means controls said switching means so that, during the search operation for said second satellite by said second demodulator, one of said first and second antennas which is connected to said second demodulator is switched to the other one of said first and second antennas.

12. A diversity type GPS according to claim 9, wherein said switching means comprises first switching means for selectively inputting a signal received from said first antenna to said first and second demodulators, and second switching means for selectively inputting a signal received from said second antenna to said first and second demodulators.

13. A diversity type GPS according to claim 12, wherein said control means further comprises means for outputting to said first and second switching means an antenna selection command for determining the input, to said first and second demodulators, of signals received from one of said first and second antennas when a search command is produced to said respective first and second demodulators.

14. A diversity type GPS according to claim 13, wherein said control means further comprises means for controlling said first and second switching means respectively, during said respective search operation of said first and second demodulators, so as to switch from a selected one of said first and second antennas to the other one of said first and second and means for continuing said search operation by using signals received from said one of said first and second antenna thus switched.

17. A diversity type GPS according to claim 12, wherein said first and second switching means comprises analog switches respectively.

18. A diversity type GPS according to claim 9, further comprising a third demodulator mounted in parallel with said first and second demodulators, and third switching means for inputting to said third demodulator signals received from said first and second antennas.

19. A diversity type GPS according to claim 9, further comprising high-frequency amplifying means for amplifying signals received from said first and second antennas and applying the amplified signals to said first and second switching means.

15. A diversity type GPS for a vehicle for computing a position of the vehicle on the basis of rf signals received from a plurality of satellites, comprising:

first and second antennas, mounted at first and second discrete positions in a compartment of a vehicle, for receiving rf signals from a plurality of satellites, and

signal receiving means for demodulating rf signals from said satellites on the basis of signals received from said first and second antennas and for computing a position of said vehicle on the basis of the demodulated data,

said signal receiving means comprising;

first and second demodulators, each for receiving a search command for a specific satellite, for performing a satellite search operation in accordance with said signals received by a selected one of said first and second antennas, and for demodulating said received signals when said search operation is effected,

switching means for selectively inputting signals received from said first and second antennas to said first and second demodulators, control means for outputting said search command for a first satellite to said first demodulator and said search command for a second satellite to said second demodulator,

computing means for computing the position of said vehicle, and wherein

said switching means comprises first switching means for selectively inputting a signal received from said first antenna to said first and second demodulators, and second switching means for selectively inputting a signal received from said second antenna to said first and second demodulators,

said control means further comprises means for outputting to said first and second switching means an antenna selection command for determining the input, to said first and second demodulators, of signals received from one of said first and second antennas when a search command is produced to said respective first and second demodulators,

said control means further comprises means for controlling said first and second switching means respectively, during said respective search operation of said first and second demodulators, so as to switch from a selected one of said first and second antennas to the other one of said first and second antennas, and means for continuing said search operation by using signals received from said one of said first and second antenna thus switched, and

said control means further comprises means for changing the switching timing of said first and second antennas in order to improve the rate of use of the one of said first and second antenna which was effective in a previous search operation when searching out the same satellite,

16. A diversity type GPS for a vehicle for computing a position of the vehicle on the basis of rf signals received from a plurality of satellites, comprising:

first and second antennas, mounted at first and second discrete positions in a compartment of a vehicle, for receiving rf signals from a plurality of satellites, and

signal receiving means for demodulating rf signals from said satellites on the basis of signals received from said first and second antennas and for computing a position of said vehicle on the basis of the demodulated data,

said signal receiving means comprising;

first and second demodulators, each for receiving a search command for a specific satellite, for performing a satellite search operation in accordance with said signals received by a selected one of said first and second antennas, and for demodulating said received signals when said search operation is effected, switching means for selectively inputting signals received from said first and second antennas to said first and second demodulators,

control means for outputting said search command for a first satellite to said first demodulator and said search command for a second satellite to said second demodulator,

computing means for computing the position of said vehicle,

a terrestrial magnetism sensor for sensing the vehicle'"'"'s direction of travel, and wherein

said switching means comprises first switching means for selectively inputting a signal received from said first antenna to said first and second demodulators, and second switching means for selectively inputting a signal received from said second antenna to said first and second demodulators,

said control means further comprises means for outputting to said first and second switching means an antenna selection command for determining the input to said first and second demodulators, of signals received from one of sad first and second antennas when a search command is produced to said respective first and second demodulators,

said control means further comprises means for controlling said first and second switching means respectively, during said respective search operation of said first and second demodulators, so as to switch from a selected one of said first second antennas to the other one of said first and second antennas, and means for continuing said search operation by using signals received from said one of said first and second antenna thus switched, and

said control means further comprises means for storing data of the rate of use of said first and second antennas on the basis of relative azimuths of said satellites relative to the direction of said vehicle, means for detecting said relative azimuth of said specific satellite, and means for changing the switching timing of said first and second antennas on the basis of said detected relative azimuth.