Classifications

• • H—ELECTRICITY
  • H04—ELECTRIC COMMUNICATION TECHNIQUE
  • H04B—TRANSMISSION
  • H04B1/00—Details of transmission systems, not covered by a single one of groups H04B3/00 - H04B13/00; Details of transmission systems not characterised by the medium used for transmission
  • H04B1/69—Spread spectrum techniques
  • H04B1/707—Spread spectrum techniques using direct sequence modulation
  • H04B1/7073—Synchronisation aspects
  • H04B1/7085—Synchronisation aspects using a code tracking loop, e.g. a delay-locked loop
• • G—PHYSICS
  • G01—MEASURING; TESTING
  • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
  • G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
  • G01S19/01—Satellite radio beacon positioning systems transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
  • G01S19/13—Receivers
  • G01S19/24—Acquisition or tracking or demodulation of signals transmitted by the system
  • G01S19/30—Acquisition or tracking or demodulation of signals transmitted by the system code related
• • H—ELECTRICITY
  • H04—ELECTRIC COMMUNICATION TECHNIQUE
  • H04J—MULTIPLEX COMMUNICATION
  • H04J13/00—Code division multiplex systems
  • H04J13/0007—Code type
  • H04J13/0022—PN, e.g. Kronecker

Definitions

• This invention relates to a method of code phase tracking for code division multiple access (CDMA) type communication and to apparatus for the same.
• CDMA code division multiple access
• GPS global positioning systems
• GPS is most notably associated with the Navigation System with Time and Ranging (NAVSTAR) GPS, an all weather, spaced based navigation system developed and operated by the US Department of Defense, however, the general principles underlying GPS are universal and not merely limited to NAVSTAR. Accordingly, GPS hereafter refers to any global positioning system comprising a plurality of CDMA radio transmitters at different locations and a receiver which determines its location based on the time of arrival of the transmissions of the radio transmitters.
• NAVSTAR Navigation System with Time and Ranging
• a GPS receiver may implement a pseudorandom noise (PRN) code correlation loop in which early (E), prompt (P) and late (L) replica codes of satellite PRN codes are continuously generated, and compared to the incoming satellite PRN codes as received by the receiver.
• PRN pseudorandom noise
• Using a code phase discriminator calculated as a function of the correlation it is then possible to determine whether a target incoming code has been acquired; if the code phase discriminator exceeds a predetermined threshold level, the target incoming code and the locally generated replica codes can be assumed to be in phase, i.e. the code is acquired. If not, the code generator produces the next series of replicas with a phase shift, typically of one chip, and the code phase discriminator is recalculated. Assuming carrier phase lock, a linear code sweep should eventually result in the target incoming code being in phase with that of the locally generated replica codes and therefore, if detected, code acquisition.
• PRN pseudorandom noise
• a code phase lock loop may be used to track the code, typically employing an early-minus-late code correlation function in order to determine the code phase error between the target incoming code and the locally generated replica codes.
• code phase shift is the basis for pseudorange measurements, the accuracy to which the pseudoranges can be measured and ultimately to which the position of the GPS receiver can be estimated depends on the accuracy to which the code phase lock loop can determine the code phase error.
• a method of code phase tracking is provided together with a receiver comprising an antenna and a signal processor for the same.
• the method comprises the steps of:
• the early-minus-late correlation function may be modified after its derivation or, alternatively, prior to its derivation by modifying either the subject signal, the early and late replica code signals or the early and late correlation values.
• Modifying any one of the parameters from which the early-minus-late correlation function is derived may enable the necessary signal processing to be simplified.
• modification of the subject signal may be achieved using relatively simple front-end analogue circuitry and modification of the early and late replica code signals may be achieved either by processing unmodified replica signals, say by filtering, or by direct generation of the appropriate sequence, especially if done in the digital domain.
• Modification of the subject signal and / or the early and late replica code signals preferably includes modification of their respective power spectrums by at least one of the following: reducing in size or removing at least one odd harmonic; increasing in size at least one even harmonic; and truncating the bandwidth between harmonics so as to excise an adjacent even harmonic.
• the invention further provides a receiver comprising a signal processor for modifying the power spectrum of a received subject signal containing a target pseudorandom noise code whereby the power spectrum of the subject signal has either at least one odd harmonic which is reduced in size or removed; at least one even harmonic which is increased in size; or a reduced bandwidth which is truncated between harmonics so as to excise an adjacent even harmonic.
• the invention yet further provides a receiver comprising an antenna for receiving a subject signal containing a target pseudorandom noise code; and a signal processor comprising a generator for generating a series of signals containing early and late replica codes corresponding to the target code, a correlator for correlating the subject signal with the early and late replica code signals and returning respective early and late correlation values, and means for determining the code phase error between the target code and the replica codes from a modified early-minus-late correlation function derived from the early and late correlation values, such that the gradient of the modified early- minus-late correlation function at zero code phase error is increased compared to the true early-minus-late correlation function.
• the above receiver may modify the early-minus-late correlation function by modifying either the subject signal, the early and late replica code signals or the early and late correlation values prior to deriving the early-minus-late correlation function.
• the receiver may modify the early-minus-late correlation function by modifying the subject signal or the early and late replica code signals whereby either or both of their respective power spectrums have either at least one odd harmonic which is reduced in size or removed; at least one even harmonic which is increased in size; or a reduced bandwidth which is truncated between harmonics so as to excise an adjacent even harmonic.
• Figure 1 shows, schematically, an SPS GPS receiver according to the present invention
• Figure 2 shows, schematically, the receiver channels and receiver processor of the GPS receiver of figure 1 in greater detail
• Figure 3 is a graph showing an idealised early-minus-late correlation function for 1.0 MHz and 4.0 MHz bandwidths
• Figure 4 is a graph showing the gradient of the early-minus-late correlation function plotted against the bandwidth of the incoming signal for both unmodified and modified incoming signals
• Figures 5A and 5B are graphs showing normalised power spectrums for both an unmodified and a modified incoming signal respectively.
• each NAVSTAR GPS satellite transmits two carrier frequencies; L1 , the primary frequency at 1575.42 MHz and L2, the secondary frequency at 1227.60 MHz.
• the carrier frequencies are modulated by spread spectrum codes with a PRN sequence unique to each satellite and also by the navigation data message.
• the L1 signal is modulated the coarse / acquisition (C/A) code and the precision (P[Y]) code whereas the L2 signal is modulated by the P[Y] code only.
• FIG. 1 shows, schematically, the architecture of an SPS GPS receiver according to the present invention.
• GPS radio frequency (RF) signals are received by an antenna 10 and pre-processed in a pre-processor 11 by preamplification, passive bandpass filtering in order to minimise out-of-band RF interference, further filtering to filter out first harmonics of the power spectrum of the incoming signal; down converting to an intermediate frequency (IF) and analog to digital conversion.
• RF radio frequency
• Digitised IF signals are then provided to each of n digital receiver channels 12 in which they are acquired and tracked in co-operation with the receiver processor 13 for the purpose of acquiring navigation information.
• Such methods for acquisition and tracking are well known, for example, see chapter 4 (GPS satellite signal characteristics) & chapter 5 (GPS satellite signal acquisition and tracking), Kaplan ibid.
• the navigation processor 14 uses acquired navigation information and the time of arrival of the transmissions, calculates the position of the receiver using conventional algorithms and that position is displayed on a display 15 to the user.
• the pre-processor 11 will be typically implemented in the form of front end analogue circuitry with the digital receiver channels 12, the receiver processor 13 and the navigation processor 14 implemented in the form of a general purpose microprocessor or a microprocessor embedded in a GPS application specific integrated circuit (ASIC).
• ASIC application specific integrated circuit
• FIG. 2 shows, schematically, the receiver channel co-operating with the receiver processor in greater detail.
• a carrier wave CW
• I in-phase
• Q quadrature phase
• the replica carrier waves ideally have the same frequency as the received signal, however, due to Doppler shift caused by the relative movement between the receiver and orbiting satellites, the frequency of the GPS signals as received in the receiver normally differs from the precise satellite transmission frequency.
• a conventional carrier wave phase lock loop is employed. Although perhaps undesirable, it is possible to omit the carrier phase lock stage altogether as the Doppler shift of the carrier and its associated effect on the code phase discriminator is reasonably small.
• E early (E), prompt (P) and late (L) replica codes of the PRN sequences are continuously generated by a code generator 22 at a frequency related to the received carrier (i.e. nominal plus Doppler).
• the replica codes are then correlated with the I and Q signals to produce three in-phase correlation components (IE, IL, IP) and three quadrature phase correlation components (QE, QL, QP), typically by integration in an integrator 23 over substantially the whole of the PRN code.
• IE in-phase correlation components
• QE quadrature phase correlation components
• QL quadrature phase correlation components
• a code phase discriminator is calculated as a function of the correlation components on which a threshold test is applied and a phase match declared if the code phase discriminator is high.
• the code generator produces the next series of replicas with single chip phase advance and the code phase discriminator is recalculated. Any declared phase match is validated by recalculating the discriminator. A linear phase sweep will eventually result in the incoming PRN code being in phase with that of the locally generated replica and thus code acquisition.
• a code phase lock loop employing an early- minus-late correlation function is used to track the code.
• the early-minus-late correlation function is modified compared to the true early-minus-late correlation function because of the aforementioned filtering out of the first harmonics of the power spectrum of the incoming signal.
• the code phase lock loop provides an enhanced code phase error signal relating to the time difference between the incoming signal and the two local generated replicas.
• the inventor believes the following analysis explains the relationship between the accuracy to which the code phase lock loop can determine the code phase error, the gradient of the early-minus-late correlation function at zero code phase error and the aforementioned power spectrum manipulation.
• the code loop error (after averaging for noise) must be to within 3.3ns, or about 1/300 T c where T c is the GPS L1 C/A signal chip period.
• Curves 31 and 32 of figure 3 shows the true, normalised, early-minus- late (E-L) correlation function for signal bandwidths of 1.0 MHz and 4.0 MHz respectively where the E-L correlation is normalised by the prompt (P) correlation value.
• E-L early-minus- late
• P prompt
• ⁇ t code phase tracking error
• n is the magnitude of the effective noise
• a finite length pseudorandom noise code may be approximated to an ideal random binary code. Accordingly, there is no periodicity of the correlation and therefore no line quantisation of the correlation power spectrum.
• the power spectrum of the correlation is given by the Fourier transform of the correlation power. Since there is no Fourier transform of a truly random binary code, in order to obtain the power spectrum, the Fourier transform of the autocorrelation function is calculated. For a binary code having an amplitude of ⁇ A, the autocorrelation function is the classic triangular shape with a base length of ⁇ 1 code chip and a maximum correlation power of A 2 . This can be expressed as follows:
• T c the chip period for the C/A code
• the correlation power can be derived from the inverse Fourier transform of the correlation power spectrum, it is therefore possible to use the power spectrum as a starting point for the derivation of the correlation function shape and size. Also, the power spectrum can be modified to reflect the consequences of any front-end filter characteristics and the Fourier transform taken of the resulting spectrum to derive the correlation characteristics. Although this does not take account of several significant effects, such as the low resolution ADC in an actual system, the qualitative results appear to be consistent with theorised models.
• an idealised power spectrum is first generated over a range of frequencies (say +8MHz or +12MHz in 0.02MHz steps) and held in a vector.
• the vector can then be "filtered” by multiplying individual elements by a transmission factor.
• the simplest form of filtering only uses filter transmissions of zero or one.
• the power spectrum is normalised to an amplitude, A, of unity.
• the precise correlation can then be generated from the power spectrum by taking the inverse Fourier transform.
• This is a vector containing the correlation as a function of time, expressed in terms of the chip period T c .
• the total length of the vector i.e. the range of time
• the correlation step size is inversely proportional to the total range of the power spectrum.
• the early-minus-late correlation can be generated by a sparse matrix operation on the precise correlation vector.
• EL(t) is a column vector containing the (E-L) correlation result
• P(t) is a column vector containing the precise correlation result
• M ( E-D is a square matrix whose dimension is the same as the vector lengths.
• the matrix M ( E.L ) is mainly zero but contains elements of ⁇ 1 on diagonals which perform the (E-L) arithmetic operation. An example is shown below:
• curve 41 shows the FOM, i.e. the gradient of the early- minus-late correlation function, varying with the half-bandwidth of incoming signal. This is due to the shape of the correlation peak being modified by the varying sum of its Fourier components.
• the reason for the variation in FOM with bandwidth is further explained by the power spectrum of the correlation described by curve 51 in figure 5A.
• the power spectrum has nulls at 1,2,3...n MHz. Between 0 and 1 MHz, even Fourier components contribute to the power, between 1 and 2 MHz odd Fourier components contribute to the power (etc.).
• the pre-processing, receiver channel and receiver processor will typically be implemented in the form of front end analogue circuitry combined with either a general purpose microprocessor or a microprocessor embedded in a GPS application specific integrated circuit.
• Implementation of a method of code phase tracking according to the present invention may be accomplished by appropriate analogue circuitry design and / or microprocessor programming.
• design and programming is well known and would be accomplished by one of ordinary skill in the art of GPS and CDMA communication without undue burden.

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• Engineering & Computer Science (AREA)
• Computer Networks & Wireless Communication (AREA)
• Radar, Positioning & Navigation (AREA)
• Remote Sensing (AREA)
• Signal Processing (AREA)
• Physics & Mathematics (AREA)
• General Physics & Mathematics (AREA)
• Position Fixing By Use Of Radio Waves (AREA)
• Synchronisation In Digital Transmission Systems (AREA)
• Radar Systems Or Details Thereof (AREA)

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• 2000
  • 2000-05-13 GB GBGB0011493.4A patent/GB0011493D0/en not_active Ceased
• 2001
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• 2005
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