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 Digital direct sequence spread spectrum receiver

Details
Inventors: Nuytkens, Peter;
Assignee: The Charles Stark Draper Laboratory, Inc. (Cambridge, MA)
Primary Examiner: Cangialosi; Salvatore
Assistant Examiner:
Attorney, Agent or Firm: Lahive & Cockfield

A direct sequence spread spectrum receiver for receiving an RF carrier radio signal modulated with a message signal in accordance with a code having a fundamental frequency converts the received signal to an IF signal centered about a frequency f.sub.o corresponding to the code fundamental frequency offset by a Doppler shift. The IF signal is digitized and sampled at a local clock frequency to develop N-bit digital signals. Locally generated digital phase shifted sine and cosine signals at frequency f.sub.o are multiplied by a local code to obtain local 1-bit IF signals which are then correlated with the digitized IF signals to develop in phase and quadrature component signals. A tracker uses the component signals to translate the frequency of the digital local IF signal to track the Doppler shift, to maintain the local sampling frequency at 4f.sub.o, and to maintain the local code generator in synchrony with the code of the received signal. Except for the IF down conversion, the receiver employs all digital circuitry. The receiver architecture is adapted to a low power sequential tracking microreceiver.

DETAILED DESCRIPTION OF ILLUSTRATED EMBODIMENTS FIG.
1 shows a block diagram of a direct sequence spread spectrum receiver according to the present invention having an RF signal converter 1, a digitizing IF signal sampler 2, a code demodulating signal extractor 3, and a data processing signal tracking section 4.
A particular embodiment will be described, by way of illustration, for receiving GPS navigational positioning signals.
In this embodiment, the receiver receives an L.
sub.
1 band signal at 1575.
42 MHz and an L.
sub.
2 band signal at 1227.
6 MHz.
The signal converting stage 1 performs IF down conversion and includes an amplifier 6 followed by a first local oscillator section 5 where the amplified received signal is mixed with the local oscillator signal at a frequency of 1401.
51 MHz to provide a signal at a common IF frequency of 173.
91 MHz for both the L.
sub.
1 and L.
sub.
2 satellite signals.
This IF signal is filtered by filter 7, and amplified by amplifier 8.
It then passes through a second local oscillator stage 9 where it is mixed with a local oscillator signal at 161.
41 MHz to form an IF signal centered at 12.
5 MHz.
The second local oscillator frequency is selected to obtain an IF signal at a frequency slightly greater then the 10 MHz GPS code frequency offset by the maximum expected carrier Doppler.
At any given time, the actual IF frequency thus varies directly with the Doppler shift.
This IF frequency is denoted f.
sub.
o.
The signal then passes through a 20 MHz low pass filter 10 as an amplified IF output signal on line 11.
The IF signal at frequency f.
sub.
o is then sampled and digitized at a sampling frequency f.
sub.
s by A/D converter 2 to form a received N-bit digital IF signal.
For purposes of a commercial GPS receiver of moderate accuracy, useful for example in general aviation and small boat navigation, as few as 4-bit signals (3 amplitude bits and 1 sign bit) may be used, although preferably higher-accuracy 6- or 8-bit A/D conversion is employed.
The N-bit digitized signals are sent to first and second signal discrimination stages 3a, 3b of the signal extractor section 3 to develop in phase and quadrature tracking component signals



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