GPS HDL Acquisition and Tracking Using C/A Code
This example shows how to acquire and track multiple global positioning system (GPS) satellite signals from a GPS baseband waveform using Simulink® blocks that are optimized for HDL code generation and hardware implementation. You use the L1 Coarse/Acquisition (C/A) code in the input waveform to perform signal acquisition and track the satellites. In acquisition, you detect the satellite signals in the waveform and estimate the coarse Doppler and C/A code phase offsets for the detected satellites. In tracking, you fine-tune the estimates and correct them to recover the legacy navigation (LNAV) symbols. The LNAV symbols can be used for GPS position estimation.
The model that you use in this example mainly consists of acquisition and tracking modules. The input to the model is a GPS baseband waveform with a sample rate of 32.768 Msps. This signal contains multiple satellite waveforms with Doppler offsets, code phase offsets, and additive white gaussian noise (AWGN) noise in it. The model upsamples the GPS waveform by a factor of six and increases the clock from 32.768 MHz to 196.6 MHz to achieve faster acquisition.
The Acquisition block decimates the GPS waveform from 32.768 Msps to 4.096 Msps and operates at this lower sampling rate. This block detects the satellites and generates coarse estimates for them.
The Tracking block uses the GPS waveform at 32.768 Msps, the pseudorandom noise identifier (PRNID) of the detected satellites, and the coarse estimates to track the satellites. At least four satellites are required for GPS position estimation, so tracking does not start until the acquisition process detects four satellites. The Tracking block contains eight instances of tracking logic to simultaneously track eight satellites. The Tracking block uses phase-locked loop, frequency-locked loop, and delay-locked loop to recover the pi/2-BPSK modulated LNAV symbols of each detected satellite. This figure shows an overview of the example model.
This example uses one Simulink model, two functions, and two scripts.
gpshdlAcquisitionTracking— Model to acquire signals and track satellites.
gpshdlAcquisitionAndTrackingUsingCACodeInit— Generates all the parameters and inputs required to run the
gpshdlAcquisitionTrackingmodel. The model calls this script in the
gpshdlAcquisitionAndTrackingUsingCACodeParameters— Generates the parameters required to run the model. The model calls this function in the
gpshdlGenerateRxInput— Generates the input GPS waveform for the receiver. The model calls this function in the
gpshdlAcquisitionTrackingValidate— Validates the outputs of the model and plots them for visualization. The model calls this function in the
This figure shows the structure of the
dataIn — Input data, specified as 18-bit complex data.
validIn — Control signal to validate the dataIn signal, specified as a Boolean scalar.
reset — Control signal to reset the receiver. The receiver restarts from acquisition.
The output ports are vectors of length 8 because the example tracks eight satellites simultaneously.
lnavSym — Legacy navigation symbols in the input waveform, returned as 16-bit complex data.
validOut — Control signal to validate all the output ports, returned as a Boolean signal.
PRNID — PRNIDs of detected satellites, returned as a 6-bit unsigned integer.
coarseDopplerOffset — Estimated coarse Doppler offset of the detected satellites, returned as a 16-bit integer.
fineDopplerOffset — Estimated fine Doppler offset of the detected satellites, returned as 25-bit real data.
coarseCodePhOffset — Estimated coarse C/A code phase offset of the detected satellites, returned as 20-bit real data.
fineCodePhOffset — Estimated fine C/A code phase offset of the detected satellites, returned as 20-bit real data.
Input Configuration subsystem to configure the transmitter parameters and channel impairments.
Number of LNAV data bits — Number of LNAV data bits to generate transmitter waveform. Use a minimum of eight bits to ensure successful tracking convergence.
Number of satellites — Number of satellites to include in the transmitter waveform, specified as an integer in the range [1,8].
Satellite PRNIDs — PRNIDs of satellites. This value must be a column vector of size equal to number of satellites. Each PRNID must be an integer in the range [1,32].
SNR (in dB) — Signal-to-noise ratio (SNR) of individual satellites in the transmitter waveform, in dB, specified as a column vector of size equal to the number of satellites. The minimum SNR value must be -20 dB.
Peak Doppler offset — Maximum Doppler offset to introduce in the satellite waveform, in Hz, specified as a column vector of size equal to the number of satellites. Each entry of this vector must be in the range [–10000, 10000].
Doppler rate — Rate of change of the Doppler offset, specified in Hz/sec, specified as a column vector of size equal to the number of satellites. Each entry of this vector must be no greater than 1000.
C/A code phase offset — C/A code delay to introduce in the waveform, specified as a column vector of size equal to the number of satellites. Each entry of this vector must be in the range (–1023, 1023).
This figure shows the
Acquisition and Tracking subsystem. This subsystem consists of the
Time Synchronization, and
Acquisition subsystem accepts the GPS waveform at a sampling rate of 32.768 Msps, decimates it to 4.096 Msps, and stores one millisecond duration of the decimated waveform. The subsystem selects coarse Doppler frequencies sequentially from -10 kHz to 10 kHz in steps of 1 kHz, generates local carrier waveforms at these frequencies, compensates for these frequencies in the decimated waveform, and outputs carrier-wiped-off waveform. The subsystem converts the carrier-wiped-off waveform into the frequency domain using a 4096-point fast Fourier transform (FFT). The subsystem fetches the frequency-domain C/A code from a look-up table (LUT) and correlates it with the waveform to find the correlation peak. When the peak is greater than a dynamic threshold, the subsystem detects the satellite with the C/A code. The corresponding Doppler frequency and C/A code phase are the coarse estimates of the satellite. The subsystem performs this frequency-domain correlation for four satellites in parallel and for eight sequential searches to finish searching all 32 GPS satellites. The subsystem then sorts and selects the eight detected satellites with the strongest correlation peaks. The subsystem also generates a 1 ms epoch signal, which asserts, for every 1 ms, to use that signal for time synchronization.
Acquisition subsystem contains these main subsystems:
Control Acquisition— Generates control signals to start acquisition and selects the satellite PRNIDs to search.
Decimation— Decimates the input waveform from 32.768 Msps to 4.096 Msps using cascaded integrator comb (CIC) and finite impulse response (FIR) decimation.
RAM Read and Write— Writes one millisecond of decimated waveform to the RAM and reads the waveform multiple times from the RAM until acquisition finishes.
Carrier Wipeoff— Generates the local waveform at coarse Doppler frequencies using a numerically controlled oscillator (NCO) and compensates for the Doppler frequencies in the decimated waveform to output carrier-wiped-off waveform.
Correlation— Performs frequency-domain correlation of the carrier-wiped-off waveform with four satellite C/A codes simultaneously. This subsystem also finds correlation peaks, generates a threshold, and compares the peaks with the threshold to detect satellites.
Sort and Prepare Outputs— Sorts the PRNIDs, coarse Doppler frequencies, and coarse code phase offset values of the detected satellites in decreasing order of their correlation peaks and outputs the eight satellites with the strongest peaks.
Time Synchronization Subsystem
Time Synchronization subsystem accepts the GPS waveform, the detected satellite PRNIDs, coarse Doppler frequencies, coarse code phase offsets, and the 1 ms epoch signal from the
Acquisition subsystem. The
Time Syncrhonization subsystem synchronizes the input GPS waveform after the
Acquisition subsystem finishes detecting the satellites and when the incoming 1 ms epoch signal asserts.
Tracking subsystem tracks the satellites detected through acquisition. The subsystem accepts the time-synchronized waveform at 32.768 Msps, the detected satellite PRNIDs, coarse Doppler offsets, and code phase offsets. The subsystem uses the coarse Doppler estimate and phase estimate to generate a local carrier using an NCO, removes the Doppler offset from the waveform, and returns a carrier-wiped-off waveform. The subsystem uses the detected PRNID and the coarse code phase offset to fetch replica C/A code from an LUT. The subsystem generates early, prompt, and late versions of this C/A code to correlate with the carrier-wiped-off waveform. The subsystem integrates these correlated outputs for every 1 millisecond (predetection integration time) and returns integrated samples after every millisecond. The integrated prompt outputs are the LNAV symbols of the receiver. The subsystem uses the integrated early and late outputs to estimate the delay error and the integrated prompt output to estimate the frequency and phase errors. The subsystem filters these errors using loop filters and feeds the filtered values to the NCO and C/A code LUT to aid local carrier generation and replica C/A code generation. This tracking logic applies to a single satellite. Similarly, the
Tracking subsystem generates eight instances of this tracking logic and tracks eight satellites simultaneously.
Tracking subsystem contains the
Tracking Core subsystem that carries out the tracking logic. The
Tracking Core subsystem contains these main subsystems:
NCO— Accepts the coarse Doppler offset and filtered fine Doppler offset. The subsystem generates a local carrier to compensate for the Doppler offset in the input waveform.
CA Code Replica— Accepts the detected satellite PRNID, coarse code phase offset, and filtered fine code phase offset to generate replica C/A code. This subsystem generates early, prompt, and late versions of the C/A code, each separated by a half C/A chip duration.
Code Wipeoff— Multiplies the carrier-wiped-off waveform with the generated early, prompt, and late C/A codes to give out code-wiped-off waveforms.
Integrate and Dump— Integrates the early, prompt, and late code-wiped-off waveforms every 1 millisecond and outputs the integrated values.
Discriminators and Loop Filters— Uses the integrated prompt value to estimate the frequency and phase errors and uses the integrated early and late values to estimate the delay error. The first- and second-order loop filters filter the generated errors to provide fine estimates.
gpshdlAcquisitionTracking model and double-click the
Input Configuration subsystem to change the transmitter configuration and channel impairments. Run the model.
Note: It may take around 25 minutes to complete the simulation.
Build Summary 0 of 1 models built (1 models already up to date) Build duration: 0h 2m 35.48s Warning: In rapid accelerator mode, when the simulation is started from the command line, visualization blocks are not updated. If the simulation is started from the toolstrip, visualization blocks are updated. Input PRNID Detected PRNID ___________ ______________ 11 11 18 18 22 22 23 23 Input code phase offset Estimated code phase offset _______________________ ___________________________ 300.34 300.17 312.88 312.7 587.21 587.04 425.89 425.69 Input doppler offset Estimated doppler offset ____________________ ________________________ 3289 3253.2 1568 1537.1 5856 5892.4 7796 7834.8
Generate HDL Code
To generate the HDL code, you must have an HDL Coder™ license. Use
makehdltb functions to generate HDL code and a HDL test bench for the
Acquisition and Tracking subsystem.
The resulting HDL code is synthesized for a Xilinx® Zynq®-7000 ZC706 evaluation board. This table shows the post place and route resource utilization. The maximum frequency of operation is 204.12 MHz.
Resources Usage _______________ _____ Slice LUT 67157 Slice Registers 68430 RAMB36 160 RAMB18 50 DSP48 233
This example uses these helper files:
. Kaplan, Elliot D., and C. Hegarty, eds., _Understanding GPS/GNSS: Principles and Applications. Third edition. GNSS Technology and Applications Series. Boston; London; Artech House, 2017.
. IS-GPS-200, Rev: L. "NAVSTAR GPS Space Segment/Navigation User Segment Interfaces." GPS Enterprise Space & Missile Systems Center (SMC) - LAAFB. https://www.gps.gov/technical/icwg/IS-GPS-200L.pdf
. Ward, P.W. "GPS Receiver Search Techniques." In Proceedings of Position, Location and Navigation Symposium - PLANS '96, 604 - 11. Atlanta, GA, USA: IEEE, 1996. https://doi.org/10.1109/PLANS.1996.509134.
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