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| United States Patent | 5663734 |
| Link to this page | http://www.wikipatents.com/5663734.html |
| Inventor(s) | Krasner; Norman F. (San Carlos, CA) |
| Abstract | A GPS receiver in one embodiment includes an antenna which receives GPS
signals at an RF frequency from in view satellites; a downconverter
coupled to the antenna for reducing the RF frequency of the received GPS
signals to an intermediate frequency (IF); a digitizer coupled to the
downconverter and sampling the IF GPS signals at a predetermined rate to
produce sampled IF GPS signals; a memory coupled to the digitizer storing
the sampled IF GPS signals (a snapshot of GPS signals); and a digital
signal processor (DSP) coupled to the memory and operating under stored
instructions thereby performing Fast Fourier Transform (FFT) operations on
the sampled IF GPS signals to provide pseudorange information. These
operations typically also include preprocessing and post processing of the
GPS signals. After a snapshot of data is taken, the receiver front end is
powered down. The GPS receiver in one embodiment also includes other power
management features and includes, in another embodiment the capability to
correct for errors in its local oscillator which is used to sample the GPS
signals. The calculation speed of pseudoranges, and sensitivity of
operation, is enhanced by the transmission of the Doppler frequency shifts
of in view satellites to the receiver from an external source, such as a
basestation in one embodiment of the invention. |
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Title Information  |
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Drawing from US Patent 5663734 |
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GPS receiver and method for processing GPS signals |
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| Publication Date |
September 2, 1997 |
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| Filing Date |
March 8, 1996 |
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Title Information  |
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References  |
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| *references marked with an asterisk below are user-added references |
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U.S. References |
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| | Reference | Relevancy | Comments | Reference | Relevancy | Comments | 5483549 Weinberg 375/151 Jan,1996 |      Your vote accepted [0 after 0 votes] | | 5420592 Johnson 342/357.12 May,1995 |      Your vote accepted [0 after 0 votes] | | 5416797 Gilhousen 370/209 May,1995 |      Your vote accepted [0 after 0 votes] | | 5379047 Yokev 342/457 Jan,1995 |      Your vote accepted [0 after 0 votes] | | 5379224 Brown 701/215 Jan,1995 |      Your vote accepted [0 after 0 votes] | | 5379320 Fernandes 375/141 Jan,1995 |      Your vote accepted [0 after 0 votes] | | 5365450 Schuchman 455/456.3 Nov,1994 |      Your vote accepted [0 after 0 votes] | | 5323163 Maki 342/357.15 Jun,1994 |      Your vote accepted [0 after 0 votes] | | 5317323 Kennedy 342/457 May,1994 |      Your vote accepted [0 after 0 votes] | | 5311194 Brown 342/357.06 May,1994 |      Your vote accepted [0 after 0 votes] | | 5271034 Abaunza 375/150 Dec,1993 |      Your vote accepted [0 after 0 votes] | | 5225842 Brown 342/357.09 Jul,1993 |      Your vote accepted [0 after 0 votes] | | 5223844 Mansell 342/357.07 Jun,1993 |      Your vote accepted [0 after 0 votes] | | 5202829 Geier 701/215 Apr,1993 |      Your vote accepted [0 after 0 votes] | | 5043736 Darnell 342/357.1 Aug,1991 |      Your vote accepted [0 after 0 votes] | | 4998111 Ma 342/352 Mar,1991 |      Your vote accepted [0 after 0 votes] | | 4959656 Kumar 342/418 Sep,1990 |      Your vote accepted [0 after 0 votes] | | 4797677 MacDoran 342/352 Jan,1989 |      Your vote accepted [0 after 0 votes] | | 4785463 Janc 375/147 Nov,1988 |      Your vote accepted [0 after 0 votes] | | 4701934 Jasper 375/147 Oct,1987 |      Your vote accepted [0 after 0 votes] | | 4601005 Kilvington 708/3 Jul,1986 |      Your vote accepted [0 after 0 votes] | | 4445118 Taylor 342/357.09 Apr,1984 |      Your vote accepted [0 after 0 votes] | | 5430759 Yokev 375/133 Dec,1969 |      Your vote accepted [0 after 0 votes] | | | | | |
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| Market Size |
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Market Review  |
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Technical Review  |
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Claims  |
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I claim:
1. A GPS receiver apparatus, comprising:
an antenna for receiving GPS signals at an RF frequency from in view
satellites;
a downconverter coupled to said antenna, said downconverter reducing the RF
frequency of said received GPS signals to an intermediate frequency (IF);
a digitizer coupled to said downconverter and receiving said IF GPS
signals, said digitizer sampling said IF GPS signals at a predetermined
rate to produce sampled IF GPS signals;
a memory coupled to said digitizer, said memory storing the sampled IF GPS
signals; and
a digital signal processor (DSP) coupled to said memory, said DSP
performing fast convolution, wherein said digital signal processor
processes said sampled IF GPS signals by performing a plurality of fast
convolutions on a corresponding plurality of blocks of said sampled IF GPS
signals to provide a plurality of corresponding results of each fast
convolution and summing a plurality of mathematical representations of
said plurality of corresponding results to obtain a first position
information.
2. A GPS receiver as in claim 1 further comprising a communication antenna
and a receiver coupled to said communication antenna and to said DSP, said
receiver for receiving a data signal containing satellite data
information.
3. A GPS receiver as in claim 2 wherein said satellite data information
comprises a Doppler information of a satellite in view of said GPS
receiver.
4. A GPS receiver as in claim 3 wherein said satellite data information
comprises an identification of a plurality of satellites in view of said
GPS receiver and a corresponding plurality of Doppler information for each
satellite of said plurality of satellites in view of said GPS receiver.
5. A GPS receiver as in claim 2 wherein said satellite data information
comprises data representative of ephemeris for a satellite.
6. A GPS receiver as in claim 1 further comprising:
a local oscillator coupled to said downconverter, said local oscillator
providing a first reference signal.
7. A GPS receiver as in claim 2 further comprising a local oscillator
coupled to said downconverter, said local oscillator providing a first
reference signal and wherein said receiver receives a precision carrier
frequency signal which is used to calibrate said first reference signal
from said local oscillator, wherein said local oscillator is used to
acquire GPS signals.
8. A GPS receiver as in claim 3 wherein said DSP compensates said sampled
IF GPS signals using said Doppler information.
9. A GPS receiver as in claim 1 further comprising a power management
circuit coupled to said downcoverter and to said digitizer, wherein after
said IF GPS signals are stored in said memory, said power management
circuit reduces power consumed by said downconverter and said digitizer.
10. A GPS receiver as in claim 8 further comprising a transmitter coupled
to said DSP, said transmitter for transmitting said pseudorange
information.
11. A GPS receiver as in claim 2 further comprising a transmitter coupled
to said DSP said transmitter for transmitting a latitude and longitude
information.
12. A method for using a GPS receiver, said method comprising:
receiving GPS signals from in view satellites;
digitizing said GPS signals at a predetermined rate to produce sampled GPS
signals;
storing said sampled GPS signals in a memory;
processing said sampled GPS signals by performing fast convolution
operations on said sampled GPS signals in said GPS receiver, wherein said
processing processes said sampled GPS signals by performing a plurality of
fast convolutions on a corresponding plurality of blocks of said sampled
GPS signals to provide a plurality of corresponding results of each fast
convolution and summing a plurality of mathematical representations of
said plurality of corresponding results to obtain a first position
information.
13. A method as in claim 12 further comprising:
receiving a data signal containing satellite data information.
14. A method as in claim 13 wherein said satellite data information
comprises a Doppler information of a satellite in view of said GPS
receiver.
15. A method as in claim 14 wherein said Doppler information is used to
compensate said sampled GPS signal and wherein said processing further
comprises preprocessing operations.
16. A method as in claim 15 wherein said first position information
comprises a pseudorange information.
17. A method as in claim 13 wherein said satellite data information
comprises data representative of ephemeris for a satellite.
18. A method as in claim 17 wherein said first position information
comprises a pseudorange information and wherein said ephemeris and said
pseudorange information are used to calculate a latitude and longitude of
said GPS receiver.
19. A method as in claim 18 wherein said latitude and longitude is
displayed to a user of said GPS receiver.
20. A method as in claim 18 wherein said latitude and longitude are
transmitted by said GPS receiver.
21. A method as in claim 12 wherein said GPS signals originate from
pseudolites.
22. A method as in claim 12 wherein said GPS signals originate from
orbiting satellites.
23. A GPS receiver as in claim 1 wherein said GPS signals originate from
pseudolites.
24. A GPS receiver as in claim 1 wherein said GPS signals originate from
orbiting satellites.
25. A method of determining pseudoranges in a global positioning satellite
(GPS) receiver, comprising:
receiving GPS signals from one or more in view GPS satellites utilizing an
antenna coupled to a downconverter, said GPS signals comprising
pseudorandom sequences;
buffering the received GPS signals in a digital snapshot memory;
processing the buffered GPS signals for one or more of the in view GPS
satellites in a digital signal processor by:
breaking the buffered data into a series of contiguous blocks whose
durations are equal to a multiple of the frame period of the pseudorandom
(PN) codes contained within the GPS signals,
for each block, creating a compressed block of data with length equal to
the duration of a pseudorandom code period by adding together successive
subblocks of data, said subblocks having duration equal to one PN frame,
such that the corresponding sample numbers of each of the subblocks are
added to one another;
for each compressed block, performing a convolution of the compressed
block's data against the pseudorandom sequence (PRS) of the GPS satellite
being processed, said convolution being performed using fast convolution
algorithms, said convolution producing a result;
performing a magnitude-squared operation on the results created from each
of said convolutions to produce magnitude-squared data;
combining said magnitude-squared data for all blocks into a single block of
data by adding together such blocks of magnitude-squared data, such that
the corresponding sample numbers of each of the magnitude-squares from the
convolution are added to one another; and
finding the location of the peak of said single block of data to high
precision using digital interpolation methods, where the location is the
distance from the beginning of the data block to the said peak, and the
location represents a pseudorange to a GPS satellite corresponding to the
PRS being processed.
26. The method of claim 25 wherein the fast convolution algorithm used in
processing the buffered GPS signals is a Fast Fourier Transform (FFT) and
the result of the convolution is produced by computing the product of the
forward transform of said compressed block and a prestored representation
of the forward transform of the PRS to produce a first result and then
performing an inverse transformation of said first result to recover said
result.
27. The method of claim 25 wherein the fast convolution algorithm used in
processing the buffered GPS signals is a Winograd algorithm.
28. The method of claim 26 wherein the effects of Doppler induced time
delays and local oscillator induced time errors are compensated for on
each compressed block of data by inserting between the forward and inverse
Fast Fourier Transform operations, the multiplication of the forward FFT
of said compressed blocks by a complex exponential whose phase versus
sample number is adjusted to correspond to the delay compensation required
for said block.
29. The method of claim 25 wherein the digital signal processor is a
general purpose programmable digital signal processing chip which is
executing stored instructions.
30. The method of claim 25 wherein the fast convolution algorithm used in
processing the buffered GPS signals is a Agarwal-Cooley algorithm.
31. The method of claim 25 wherein the fast convolution algorithm used in
processing the buffered GPS signals is a split nesting algorithm.
32. The method of claim 25 wherein the fast convolution algorithm used in
processing the buffered GPS signals is a recursive polynomial nesting
algorithm.
33. The method of claim 25 further including the step of:
determining that said peak is valid by determining whether said peak
exceeds a predetermined threshold.
34. A tracking process utilizing global positioning system (GPS) satellites
for determining the position of a remote sensor, the process comprising
the steps of:
receiving and storing GPS signals at said remote sensor from a plurality of
in view GPS satellites;
computing pseudoranges in the sensor utilizing said GPS signals, said
computing comprising digital signal processing representations of said GPS
signals by performing a plurality of fast convolutions on a corresponding
plurality of blocks of data representing said GPS signals to provide a
plurality of corresponding results of each fast convolution and summing a
plurality of mathematical representations of said plurality of
corresponding results to obtain a first position information;
transmitting said pseudoranges from said sensor to a base station, said
base station being provided with GPS satellite ephemeris data; and
receiving said pseudoranges at said base station and utilizing said
pseudoranges and said satellite ephemeris data to compute a geographic
location for said sensor.
35. A tracking process utilizing global positioning system (GPS) satellites
for determining the position of a remote sensor, the process comprising
the steps of:
receiving and storing GPS signals at said remote sensor from a plurality of
in view GPS satellites;
computing pseudoranges in the sensor, utilizing said GPS signals, said
computing comprising digital signal processing using fast convolution
techniques on stored GPS signals;
transmitting said pseudoranges from said sensor to a base station, said
base station being provided with GPS satellite ephemeris data; and
receiving said pseudoranges at said base station and utilizing said
pseudoranges and said satellite ephemeris data to compute a geographic
location for said sensor, wherein the step of computing the pseudoranges
comprises:
storing the received GPS signals in a memory;
processing the stored GPS signals for one or more of the in view GPS
satellites in a digital signal processor by:
breaking the stored data into a series of contiguous blocks whose durations
are equal to a multiple of the frame period of the pseudorandom (PN) codes
contained within the GPS signals;
for each block, creating a compressed block of data with length equal to
the duration of a pseudorandom code period by coherently adding together
successive subblocks of data, said subblocks having duration equal to one
PN frame;
for each compressed block, performing a matched filtering operation to
determine the relative timing between the received PN code contained
within the block of data and a locally generated PN reference signal, said
matched filtering operation utilizing said fast convolution techniques;
and
determining said pseudorange by performing a magnitude-squared operation on
the products created from said matched filtering operation and combining
said magnitude-squared data for all blocks into a single block of data by
adding together said blocks of magnitude-squared data to produce a peak,
the location of said peak being determined using digital interpolation
methods and corresponding to said pseudorange.
36. The tracking process of claim 35 wherein said matched filtering
operation comprises:
performing a convolution of the compressed block's data against the
pseudorandom sequence (PRS) of the GPS satellite being processed, said
convolution being performed using said fast convolution algorithms to
produce a product of the convolution.
37. The tracking process of claim 36 wherein the fast convolution algorithm
used in processing the buffered GPS signals is a Fast Fourier Transform
(FFT) and the product of the convolution is produced by computing the
forward transform of said compressed block by a prestored representation
of the forward transform of the PRS to produce a first result and then
performing an inverse transformation of said first result to recover said
product.
38. A method as in claim 12 wherein said GPS signals were sampled at a rate
of a multiple of 1.024 MHz to provide said sampled GPS signals.
39. A GPS receiver as in claim 1 wherein said predetermined rate is a
multiple of 1.024 MHz.
40. A GPS receiver as in claim 1 wherein said DSP also performs a
preprocessing operation.
41. A GPS receiver as in claim 40 wherein said preprocessing operation
occurs before said fast convolutions.
42. A GPS receiver as in claim 41 wherein said preprocessing operation
comprises correcting for Doppler shift of signals from said view
satellite.
43. A GPS receiver as in claim 41 wherein said preprocessing operation
comprises adding together portions of said sampled IF GPS signals to
provide at least one of said corresponding plurality of blocks of said
sampled IF GPS signals.
44. A GPS receiver as in claim 43 wherein said plurality of mathematical
representations comprises a plurality of squares of magnitudes.
45. A process utilizing global positioning system (GPS) satellites for
determining the position of a remote sensor, the process comprising the
steps of:
receiving and storing GPS signals at said remote sensor from a plurality of
in view GPS satellites;
computing pseudoranges in the sensor utilizing said GPS signals, said
computing comprising digital signal processing representations of said GPS
signals by performing a plurality of fast convolutions on a corresponding
plurality of blocks of data representing said GPS signals to provide a
plurality of corresponding results of each fast convolution and summing a
plurality of mathematical representations of said plurality of
corresponding results to obtain a first position information;
receiving a transmission of satellite data information comprising data
representative of ephemeris for a plurality of satellites;
computing position information in the sensor by using said satellite data
information and said pseudoranges.
46. A process as in claim 45 wherein said transmission comes from a
basestation.
47. A process as in claim 45 wherein said transmission comprises
transmissions from said plurality of satellites.
48. A process as in claim 45 wherein said position information is
transmitted to a basestation.
49. A process as in claim 51 further comprising receiving a precision
carrier frequency signal from said basestation; automatically locking to
said precision carrier frequency signal from said basestation; and
calibrating a local oscillator in said remote sensor with said precision
carrier frequently signal.
50. A process as in claim 47 wherein said remote sensor comprises a GPS
receiver which receives said transmissions comprising data representative
of ephemeris for a plurality of satellites.
51. A process utilizing global positioning system (GPS) satellites for
determining the position of a remote sensor, the process comprising the
steps of:
receiving and storing GPS signals at said remote sensor from a plurality of
in view GPS satellites;
computing pseudoranges in the sensor, utilizing said GPS signals, said
computing comprising digital signal processing using fast convolution
techniques on stored GPS signals;
receiving a transmission of satellite data information comprising data
representative of ephemeris for a plurality of satellites;
computing position information in the sensor by using said satellite data
information and said pseudoranges, wherein the step of computing the
pseudoranges comprises:
storing the received GPS signals in a memory;
processing the stored GPS signals for one or more of the in view GPS
satellites in a digital signal processor by:
breaking the stored data into a series of contiguous blocks whose durations
are equal to a multiple of the frame period of the pseudorandom (PN) codes
contained within the GPS signals;
for each block, creating a compressed block of data with length equal to
the duration of a pseudorandom code period by coherently adding together
successive subblocks of data, said subblocks having duration equal to one
PN frame;
for each compressed block, performing a matched filtering operation to
determine the relative timing between the received PN code contained
within the block of data and a locally generated PN reference signal, said
matched filtering operation utilizing said fast convolution techniques;
and
determining said pseudorange by performing a magnitude-squared operation on
the products created from said matched filtering operation and combining
said magnitude-squared data for all blocks into a single block of data by
adding together said blocks of magnitude-squared data to produce a peak,
the location of said peak being determined using digital interpolation me
and corresponding to said pseudorange.
52. The process of claim 51 wherein said matched filtering operation
comprises:
performing a convolution of the compressed block's data against the
pseudorandom sequence (PRS) of the GPS satellite being processed, said
convolution being performed using said fast convolution algorithms to
produce a product of the convolution.
53. The process of claim 52 wherein the fast convolution algorithm used in
processing the buffered GPS signals is a Fast Fourier Transform (FFT) and
the product of the convolution is produced by computing the forward
transform of said compressed block by a prestored representation of the
forward transform of the PRS to produce a first result and then performing
an inverse transformation of said first result to recover said product.
54. A process as in claim 47 wherein said step of computing pseudoranges
further comprises performing a preprocessing operation before said fast
convolutions.
55. A process utilizing global positioning system (GPS) satellites for
determining the position of a remote sensor, the process comprising the
steps of:
receiving and storing GPS signals at said remote sensor from a plurality of
in view GPS satellites;
computing pseudoranges in the sensor, utilizing said GPS signals, said
computing comprising digital signal processing using fast convolution
techniques on stored GPS signals, wherein said step of computing
comprises:
performing a preprocessing operation before said fast convolution
techniques and performing a post processing operation after said fast
convolution techniques, wherein said fast convolution techniques comprise
a matched filtering operation and wherein said GPS signals are stored in a
series of contiguous blocks in a memory and wherein said preprocessing
comprises, for each block, creating a compressed block of data by adding
together successive subblocks of data, and wherein said post processing
comprises adding together a representation of the products created from
said matched filtering operation;
receiving a transmission of satellite data information comprising data
representative of ephemeris for a plurality of satellites; and
computing position information in the sensor by using said satellite data
information and said pseudoranges.
56. A process as in claim 34 further comprising receiving a precision
carrier frequency signal from said basestation; automatically locking to
said precision carrier frequency signal from said basestation; and
calibrating a local oscillator in said remote sensor with said precision
carrier frequency signal.
57. A process as in claim 34 wherein said step of computing pseudoranges
further comprises performing a preprocessing operation before said fast
convolutions.
58. A tracking process utilizing global positioning system (GPS) satellites
for determining the position of a remote sensor, the process comprising
the steps of:
receiving and storing GPS signals at said remote sensor from a plurality of
in view GPS satellites;
computing pseudoranges in the sensor, utilizing said GPS signals, said
computing comprising digital signal processing using fast convolution
techniques on stored GPS signals, wherein said step of computing
comprises:
performing a preprocessing operation before said fast convolution
techniques and performing a post processing operation after said fast
convolution techniques, wherein said fast convolution techniques comprise
a matched filtering operation and wherein said GPS signals are stored in a
series of contiguous blocks in a memory and wherein said preprocessing
comprises, for each block, creating a compressed block of data by adding
together successive subblocks of data, and wherein said post processing
comprises adding together a representation of the products created from
said matched filtering operation;
transmitting said pseudoranges from said sensor to a base station, said
base station being provided with GPS satellite ephemeris data; and
receiving said pseudoranges at said base station and utilizing said
pseudoranges and said satellite ephemeris data to compute a geographic
location for said sensor.
59. A GPS receiver as in claim 7 wherein said satellite data information
comprises an identification of a plurality of satellites in view of said
GPS receiver and a corresponding plurality of Doppler information for each
satellite of said plurality of satellites in view of said GPS receiver.
60. A GPS receiver as in claim 7 further comprising a power management
circuit coupled to said downconverter and to said digitizer, wherein after
said IF GPS signals are stored in said memory, said power management
circuit reduces power consumed by said downconveter and said digitizer. |
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Claims  |
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Description  |
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BACKGROUND OF THE INVENTION
RELATED APPLICATIONS
This application is related to two patent applications filed by the same
inventor on the same date as this application; these two applications are:
An Improved GPS Receiver Utilizing a Communication Link (Ser. No.
08/612,582); An Improved GPS Receiver Having Power Management (Ser. No.
08/613,966).
This application is also related to and hereby claims the benefit of the
filing date of a provisional patent application by the same inventor,
Norman F. Krasner, which application is entitled Low Power, Sensitive
Pseudorange Measurement Apparatus and Method for Global Positioning
Satellites Systems, Ser. No. 60/005,318, filed Oct. 9, 1995.
A portion of the disclosure of this patent document contains material which
is subject to copyright protection. The copyright owner has no objection
to the facsimile reproduction by anyone of the patent document or the
patent disclosure, as it appears in the Patent and Trademark Office patent
file or records, but otherwise reserves all copyright rights whatsoever.
1. FIELD OF THE INVENTION
The present invention relates to receivers capable of determining position
information of satellites and, in particular, relates to such receivers
which find application in global positioning satellite (GPS) systems.
2. BACKGROUND ART
GPS receivers normally determine their position by computing relative times
of arrival of signals transmitted simultaneously from a multiplicity of
GPS (or NAVSTAR) satellites. These satellites transmit, as part of their
message, both satellite positioning data as well as data on clock timing,
so-called "ephemeris" data. The process of searching for and acquiring GPS
signals, reading the ephemeris data for a multiplicity of satellites and
computing the location of the receiver from this data is time consuming,
often requiring several minutes. In many cases, this lengthy processing
time is unacceptable and, furthermore, greatly limits battery life in
micro-miniaturized portable applications.
Another limitation of current GPS receivers is that their operation is
limited to situations in which multiple satellites are clearly in view,
without obstructions, and where a good quality antenna is properly
positioned to receive such signals. As such, they normally are unusable in
portable, body mounted applications; in areas where there is significant
foliage or building blockage; and in in-building applications.
There are two principal functions of GPS receiving systems: (1) computation
of the pseudoranges to the various GPS satellites, and (2) computation of
the position of the receiving platform using these pseudoranges and
satellite timing and ephemeris data. The pseudoranges are simply the time
delays measured between the received signal from each satellite and a
local clock. The satellite ephemeris and timing data is extracted from the
GPS signal once it is acquired and tracked. As stated above, collecting
this information normally takes a relatively long time (30 seconds to
several minutes) and must be accomplished with a good received signal
level in order to achieve low error rates.
Virtually all known GPS receivers utilize correlation methods to compute
pseudoranges. These correlation methods are performed in real time, often
with hardware correlators. GPS signals contain high rate rep | | |