# Patent

## Title
Circuits and methods for detecting interferers

## Abstract

Mechanisms for interferer detection can detect interferers by detecting elevated signal amplitudes in one or more of a plurality of bins (or bands) in a frequency range between a maximum frequency (fMAX) and a minimum frequency (fMIN). To perform rapid interferer detection, the mechanisms downconvert an input signal x(t) with a local oscillator (LO) to a complex baseband signal xI(t)+jxQ(t). xI(t) and xQ(t) are then multiplied by m unique pseudorandom noise (PN) sequences (e.g., Gold sequences) gm(t) to produce m branch signals for I and m branch signals for Q. The branch signals are then low pass filtered, converted from analog to digital form, and pairwise combined by a pairwise complex combiner. Finally, a support recovery function is used to identify interferers.

## Background
CROSS-REFERENCE TO RELATED APPLICATION
This application claims the benefit of U.S. Provisional Patent Application No. 62/236,959, filed Oct. 4, 2015, and is a continuation in part of Patent Cooperation Treaty Application No. PCT/US2015/050058, filed Sep. 14, 2015, which claims the benefit of U.S. Provisional Patent Application No. 62/049,785, filed Sep. 12, 2014, each of which is hereby incorporated by reference herein in its entirety.


STATEMENT REGARDING GOVERNMENT FUNDED RESEARCH
This invention was made with government support under Grant #: ECCS-1343282 awarded by the National Science Foundation. The government has certain rights in the invention.


BACKGROUND
As more and more devices utilize radio frequency techniques to effect wireless communication and control, available spectral resources become fewer and fewer. In attempt to address this situation, certain techniques, such as cognitive radio, allow opportunistic use of available spectral resources.
In many of these techniques, before a device can use a certain part of the radio frequency spectrum, it is desirable for the device to first determine whether there are interferers that may interfere with the device's use of the part of the spectrum.
While certain techniques for detecting interferers exist, these techniques are slow or energy inefficient.
Accordingly, new mechanisms for detecting interferers are desired.
SUMMARY
In accordance with some embodiments, circuits and methods for detecting interferers are provided. In some embodiments, circuits for detecting interferers are provided, the circuits comprising: a first in-phase mixer that receives and mixes a radio frequency (RF) signal and an in-phase local oscillator signal to produce a first in-phase mixer output signal; a first quadrature-phase mixer that receives and mixes the radio frequency (RF) signal and a quadrature-phase local oscillator signal to produce a first quadrature-phase mixer output signal; a first in-phase filter that receives and filters the first in-phase mixer output signal and produces a first in-phase filtered signal; a first quadrature-phase filter that receives and filters the first quadrature-phase mixer output signal and produces a first quadrature-phase filtered signal; a first in-phase branch that comprises: a second in-phase mixer that receives and mixes the first in-phase filtered signal and a first pseudorandom noise signal to produce a second in-phase mixer output signal; a second in-phase filter that receives and filters the second in-phase mixer output signal to produce a second in-phase filtered signal; and a first in-phase analog-to-digital converter that receives the second in-phase filtered signal and produces a first in-phase digitized signal; a second in-phase branch that comprises: a third in-phase mixer that receives and mixes the first in-phase filtered signal and a second pseudorandom noise signal to produce a third in-phase mixer output signal; a third in-phase filter that receives and filters the third in-phase mixer output signal to produce a third in-phase filtered signal; and a second in-phase analog-to-digital converter that receives the third in-phase filtered signal and produces a second in-phase digitized signal; a first quadrature-phase branch that comprises: a second quadrature-phase mixer that receives and mixes the first quadrature-phase filtered signal and the first pseudorandom noise signal to produce a second quadrature-phase mixer output signal; a second quadrature-phase filter that receives and filters the second quadrature-phase mixer output signal to produce a second quadrature-phase filtered signal; and a first quadrature-phase analog-to-digital converter that receives the second quadrature-phase filtered signal and produces a first quadrature-phase digitized signal; a second quadrature-phase branch that comprises: a third quadrature-phase mixer that receives and mixes the first quadrature-phase filtered signal and the second pseudorandom noise signal to produce a third quadrature-phase mixer output signal; a third quadrature-phase filter that receives and filters the third quadrature-phase mixer output signal to produce a third quadrature-phase filtered signal; and a second quadrature-phase analog-to-digital converter that receives the third quadrature-phase filtered signal and produces a second quadrature-phase digitized signal; a complex combiner that combines the first in-phase digitized signal and the first quadrature-phase digitized signal to produce a first combined signal and that combines the second in-phase digitized signal and the second quadrature-phase digitized signal to produce a second combined signal; and at least one hardware processor that receives the first combined signal and the second combined signal and that identifies at least one interferer in the RF signal using the first combined signal and the second combined signal.
In some embodiments, methods for detecting interferers are provided, the methods comprising: mixing a radio frequency (RF) signal and an in-phase local oscillator signal to produce a first in-phase mixer output signal; mixing the radio frequency (RF) signal and a quadrature-phase local oscillator signal to produce a first quadrature-phase mixer output signal; filtering the first in-phase mixer output signal to produce a first in-phase filtered signal; filtering the first quadrature-phase mixer output signal to produce a first quadrature-phase filtered signal; mixing the first in-phase filtered signal and a first pseudorandom noise signal to produce a second in-phase mixer output signal; filtering the second in-phase mixer output signal to produce a second in-phase filtered signal; analog-to-digital converting the second in-phase filtered signal to produce a first in-phase digitized signal; mixing the first in-phase filtered signal and a second pseudorandom noise signal to produce a third in-phase mixer output signal; filtering the third in-phase mixer output signal to produce a third in-phase filtered signal; analog-to-digital converting the third in-phase filtered signal to produce a second in-phase digitized signal; mixing the first quadrature-phase filtered signal and the first pseudorandom noise signal to produce a second quadrature-phase mixer output signal; filtering the second quadrature-phase mixer output signal to produce a second quadrature-phase filtered signal; analog-to-digital converting the second quadrature-phase filtered signal to produce a first quadrature-phase digitized signal; mixing the first quadrature-phase filtered signal and the second pseudorandom noise signal to produce a third quadrature-phase mixer output signal; filtering the third quadrature-phase mixer output signal to produce a third quadrature-phase filtered signal; analog-to-digital converting the third quadrature-phase filtered signal to produce a second quadrature-phase digitized signal; combining the first in-phase digitized signal and the first quadrature-phase digitized signal to produce a first combined signal and combining the second in-phase digitized signal and the second quadrature-phase digitized signal to produce a second combined signal; and identifying at least one interferer in the RF signal using the first combined signal and the second combined signal.



BRIEF DESCRIPTION OF THE DRAWINGS
Various objects, features, and advantages of the disclosed subject matter can be more fully appreciated with reference to the following detailed description of the disclosed subject matter when considered in connection with the following drawings, in which like reference numerals identify like elements.
FIG. 1 is an example of a circuit for detecting interferers in accordance with some embodiments.
FIG. 2 is an example of a circuit for implementing a quadrature analog-to-information converter in accordance with some embodiments.
FIG. 3 is an example of a block diagram showing functions that can be performed by a complex combiner, a support recovery block, and a signal reconstruction block in accordance with some embodiments.
FIG. 4 is an example of a circuit for two maximal length sequence generators that can be used in accordance with some embodiments.
FIG. 5 is an example of a circuit for a Gold sequence generator that can be used in accordance with some embodiments.
FIG. 6 is an example of a circuit diagram showing theory behind a mechanism for detecting interferers, including linear impairments (I/Q phase and gain imbalance) in accordance with some embodiments.
FIG. 7 is an example of a block diagram of a compressed sampling (CS) time-segmented quadrature analog-to-information converter in accordance with some embodiments.
FIG. 8 is an example of a compressed sampling problem in accordance with some embodiments.
FIG. 9 is an example of a circuit implement of a rapid interfere detector using a compressed-sampling time-segmented quadrature analog-to-information converter (TS-QAIC) in accordance with some embodiments.
FIG. 10 is an example of an approach to selecting a sensing matrix Φ constructed from two time-segmented Gold sequence sets to detect K0=6 interferers in accordance with some embodiments.
FIG. 11 is an example of hardware that can be used to implement a support recovery block, a signal reconstruction block, a system controller and user interface, and/or any other suitable portions of the circuits described herein in accordance with some embodiments.



DETAILED DESCRIPTION
In accordance with some embodiments, mechanisms (which can include circuits, systems, methods, and computer readable media) for detecting interferers in a frequency range are provided.
The mechanisms described herein for interferer detection can detect interferers by detecting elevated signal amplitudes in one or more of a plurality of bins (or bands) in a frequency range between a maximum frequency (fMAX) and a minimum frequency (fMIN) in some embodiments. Any suitable number of bins (or bands) (which number is referred to herein as N0) can be used, and any suitable maximum and minimum frequencies can be used, in some embodiments.
Turning to FIG. 1, an example 100 of a circuit for interferer detection in accordance with some embodiments is shown. As illustrated, circuit 100 includes an antenna 104, a quadrature analog-to-information converter (QAIC) front-end 103, a local oscillator source 112, analog-to-digital converters (ADCs) 144, 146, 148, 150, 152, and 154, a complex combiner 156, a support recovery block 158, a signal reconstruction block 160, and a system controller and user interface 162.
In accordance with some embodiments, to perform rapid interferer detection, circuit 100 downconverts an input signal x(t) with a local oscillator (LO) to a complex baseband signal xI(t)+jxQ(t). xI(t) and xQ(t) are then multiplied by m unique pseudorandom noise (PN) sequences (e.g., Gold sequences) gm(t) to produce m branch signals for I and m branch signals for Q. The branch signals are then low pass filtered, converted from analog to digital form, and pairwise combined by a pairwise complex combiner. Finally, a support recovery function is used to identify interferers.
As shown in FIG. 1, QAIC front-end 103 includes a low noise amplifier (LNA) 106, mixers 108 and 110, a divide-by-two circuit 114, filters 116 and 118, mixers 120, 122, 124, 126, 128, and 130, filters 132, 134, 136, 138, 140, and 142, and a Gold sequence generator 131.
When an input signal x(t) 102 is received from antenna 104, the input signal is amplified by LNA 106. LNA 106 can be any suitable low noise amplifier in accordance with some embodiments. In some embodiments, a wideband noise-canceling low-noise amplifier can be used as LNA 106. A wideband noise-canceling low-noise amplifier can be used as LNA 106, for example, when impedance matching is required for a given instantaneous bandwidth (e.g., 1 GHz).
The output of LNA 106 is then provided to mixers 108 and 110, which mix the amplified signal with local oscillators cos(ωlot) and sin(ωlot), respectively. Mixers 108 and 110 can be any suitable mixers. For example, in some embodiments, the mixers can be current-driven passive I/Q mixers.
The local oscillators can be produced by any suitable source. For example, in some embodiments, the local oscillators can be produced by local oscillator source 112 in conjunction with divide-by-two circuit 114. Local oscillator source 112 can be any suitable source of a local oscillator signal, such as a phase lock loop synthesizer. The local oscillators can have any suitable frequency. For example, the local oscillator signal produced by source 112 can have a frequency of 6.4 GHz, and the local oscillators output by circuit 114 can be 3.2 GHz quadrature signals that have a 50% duty cycle.
The outputs of mixers 108 and 110 are filtered by filters 116 and 118 to produce xI(t) and xQ(t), respectively. Any suitable filters can be used for filters 116 and 118 in accordance with some embodiments. For example, low pass filters with a cut-off frequency of 0.5 GHz can be used for filters 116 and 118 in some embodiments.
Next, the signals xI(t) and xQ(t) output by filters 116 and 118 are provided to m branches for each of the I and Q paths for a total of M=2m branches. Any suitable number of branches can be used in some embodiments. For example, in some embodiments, the total number of branches M needed for successful signal recovery can be determined by the maximum number of supports (i.e., interferers), K0, the length of the PN sequence, L, and a constant, C according to the equation: M=C·K0·log(L/K0).
For the purposes of illustration, FIG. 1 shows one three of the m in-phase branches and three of the m quadrature-phase branches. In some embodiments, m may be equal to eight or any other suitable number. Within these three illustrative branches, the signal xI(t) is provided to mixers 120, 122, and 124, and the signal xQ(t) is provided to mixers 126, 128, and 130. Any suitable mixers can be used in some embodiments. For example, in some embodiments, the mixers can be current-driven passive I/Q mixers.
Mixers 120, 122, and 124 and mixers 126, 128, and 130 mix signals xI(t) and xQ(t), respectively, with unique Gold sequence g1(t), gm-1(t), and gm(t) for each branch m. More particularly, for example, mixers 120 and 126 mix signals xI(t) and xQ(t), respectively, with Gold sequence g1(t). As another example, mixers 122 and 128 mix signals xI(t) and xQ(t), respectively, with Gold sequence gm-1(t). As yet another example, mixers 124 and 130 mix signals xI(t) and xQ(t), respectively, with Gold sequence gm(t).
The Gold sequences can have any suitable length in some embodiments. For example, in some embodiments, the Gold sequences can have a length of 15, 31, 63 or 127.
Although FIG. 1 is described as mixing Gold sequences with xI(t) and xQ(t), any suitable pseudo random sequence (PRBS) can be used in some embodiments.
As another example, in some embodiments, maximal length PRBSs generated with linear feedback shift registers (LFSR) can be used. The sequence length L can be equal to 2r−1, where rε+ for a maximal length LFSR type PRBS. The number of shift registers r in the LFSR structure can be chosen such that L is greater than or equal to the number of bins (or bands) in the frequency range (fMAX−fMIN) (e.g., 1 GHz (3.7 GHz (fMAX)−2.7 GHz (fMIN)) to be checked for interferers and the frequency of the PRBS (fPRBS) is greater than the frequency span.
The output of mixer in each of the in-phase and quadrature phase branches (e.g., mixers 120, 122, 124, 126, 128, and 130) is filtered by a filter for that branch (e.g., one of filters 132, 134, 136, 138, 140, and 142). Any suitable filters can be used for these filters in accordance with some embodiments. For example, low pass filters with a cut-off frequency of RBW/2 (e.g., 10 MHz) can be used for these filters in some embodiments.
The output of the filters in each of the in-phase and quadrature phase branches (e.g., filters 132, 134, 136, 138, 140, and 142) is converted from analog to digital by an ADC for that branch (e.g., one of ADCs 144, 146, 148, 150, 152, and 154). Any suitable ADCs can be used for these ADCs in accordance with some embodiments, and these ADCs can have any suitable number of bits and sampling rate. For example, in some embodiments, 1 or 8 bit ADCs with sampling rates of equal to the RBW, or multiples thereof can be used.
The aggregate sampling rate for the ADCs is the number of branches multiplied by the sampling rate for each ADC. In some embodiments, the number of branches may be reduced by a factor q if the branch sampling rate is increased by a factor q to maintain the same aggregate sampling rate.
The outputs of the I and Q path branches are next pairwise added by complex combiner 156. As shown in block 302 of FIG. 3, this can be done by the complex combiner providing an output y for each pair of I and Q branches 1 through m as follows:

yi=XBBIi∓jXBBQi 

The outputs of the complex combiner y1 . . . ym are provided to support recovery block 158 and signal reconstruction block 160.
Within support recovery block 158, any suitable technique and any suitable hardware can be used to identify interferers. For example, in some embodiments, as shown in FIG. 3, the Orthogonal Matching Pursuit (OMP) technique (shown in block 304) can be used to find the input signal frequency bins (or bands) that exceed an adaptive threshold, and thus certain interferers. The OMP forms an estimate of the signal support (i.e., interferers) (active bins) one element at a time.
As also shown in FIG. 3, in addition to receiving the outputs of the complex combiner, the OMP receives stopping criteria and a measurement matrix A. Any suitable stopping criteria and measurement matrix A can be used in some embodiments. For example, in some embodiments, user specified parameters like fMAX, fMIN and resolution bandwidth (RBW) (i.e., the frequency range divided by the number of bins (or bands)) can be used to generate the measurement matrix A, and user specified performance targets like sensitivity can be used to derive the adaptive stopping criteria. This threshold can be set to optimize the detection or false alarm probabilities, PD or PFA. For example, the threshold can be set close to the noise floor to maximize performance in some embodiments.
Within signal reconstruction block 160, any suitable technique and any suitable hardware can be used to reconstruct the signal x(t). For example, as shown in FIG. 3, in some embodiments, the list (I) of active bins found by the OMP at block 304 can be used to reconstruct an estimate of the input signal x(t) at block 306. This can be done, for example, by forming a pseudoinverse of the reduced measurement matrix (AI), and solving directly for x(t) from the complex combiner output values y.
Finally, system controller and user interface 162 can be used to configure circuit 100 according to user specified system constants and performance targets such as RBW, sensitivity, maximum and minimum frequencies of interest, fMAX and fMIN, and detection and false alarm probabilities, PD and PFA.
Turning to FIG. 2, an example 203 of a circuit for QAIC front-end 103 that can be used in accordance with some embodiments is illustrated. As shown, circuit 203 includes an LNA 206, a mixer 208, a transconductance amplifier 264, DC blocking capacitors 266 and 268, a divide-by-two circuit 214, a filter 216, mixers 220 and 224, a Gold sequence generator 231, and filters 232 and 236.
As also shown in FIG. 2, circuit 203 includes an I path 205 and a Q path 207. Q path 207 includes the same components as the components in I path 205 and receives the same signals from LNA 206. However, unlike I path 205 which receives LO_0° clock signals (i.e., LO_0°+, LO_0°+b, LO_0°−, and LO_0°−b), Q path 207 receives LO_90° signals (i.e., LO_90°+, LO_90°+b, LO_90°−, and LO_90°−b).
As further shown in FIG. 2, unlike in circuit 100, the output of LNA 206 (which is differential) is connected to a differential transconductance Gm amplifier 264 (which can operate in any suitable range (e.g., such as 2.7 to 3.7 GHz)), which has its outputs connected to DC blocking capacitors 266 and 268, which are connected to differential mixer 208. Mixer 208 can be implemented in any suitable manner, such as using four pairs of CMOS transmission gate switches. In some embodiments, a non-overlap generator can be formed by two cross-coupled NAND gates with inverter chains to generate complementary phase clocks for use with transmission gate type passive mixer switches.
The output of mixer 208 is connected to filter 216, which can be implemented in any suitable manner, such as by a transimpedance amplifier that is configured as an RF I/Q filter, in some embodiments.
As still further shown in FIG. 2, circuit 203 includes I paths 209 and Q paths 211, which each include eight branches. Within each branch, there is a mixer (e.g., mixer 220 or 224) and a filter (e.g., filter 232 or 236). The input to these branches is connected to the output of filter 216 (for the I paths) or to the output of the equivalent filter (not shown) in Q path 207.
As yet further shown in FIG. 2, unlike in circuit 100, the output of filter 216 (which is differential) is connected to a differential transconductance Gm amplifier in each branch of I paths 209, the outputs of each amplifier is connected to a differential switch (in the same branch) that is controlled by one of the Gold sequences produced by Gold sequence generator 231 to form a mixer for the branch (e.g., mixer 220 or 224).
The outputs of the mixers in each branch of the I paths 209 and the Q paths 211 are connected to a filter for the branch (e.g., filter 232 or 236). These filters can be implemented in any suitable manner, such as by a transimpedance amplifier that is configured as an RF I/Q filter, in some embodiments.
As still further shown in FIG. 2, Gold sequence generator 231 can be programmable in some embodiments. This can allow the RBW to be changed to different values (e.g., between 20 MHz and 10 MHz) by switching to corresponding PN length options (e.g., between 63-long and 127-long). In some embodiments, Gold sequence generator 231 can generate 8 (2n−1) long Gold sequences by XORing two maximal length m-sequences generated by two n-flip-flop linear feedback shift registers.
As shown in FIG. 2, Gold sequence generator 231 can be clocked at L times RBW (which needs to be equal to or larger than the span) (e.g., a 1.26 GHz clock frequency). In some embodiments, any other suitable clock frequency can be used.
FIGS. 4 and 5 show further details of Gold sequence generators that can be used in some embodiments.
As shown in FIG. 4, maximal length sequence generator 1 and maximal length sequence generator 2 shown in the Gold sequence generator 231 of FIG. 2 can be implemented as maximal length sequence generator 1 402 and maximal length sequence generator 2 404, respectively, in some embodiments. By changing the configuration of switches C0, C0b, C4, C4b, C5, C6, and C7, length options of 15, 31, 63 and 127 can be programmed for the Gold sequences output by Gold sequence generator 231 as shown in table 406.
As shown in FIG. 5, in some embodiments, in an alternate version of Gold sequence generator 231, the output flip flops at the outputs of the XOR gates can be omitted and the outputs of the XOR gates provided directly to the mixers of the branches in I paths 209 and Q paths 211.
Any suitable components technologies and sizes can be used to implement the circuit devices shown in FIGS. 1, 2, 4, and 5. For example, in some embodiments, these devices can be implemented in 65 nm CMOS general purpose device technology.
Turning to FIG. 6, an alternate circuit 600 for detecting interferers in accordance with some embodiment is shown to derive a set of equations that describe the operation of the mechanisms described herein.
For the purposes of illustration, impairments of the downconverter are included in the frequency domain model and only linear impairments are considered. The downconverter frequency independent impairment model at the output of box 608 can be described as follows:




  
    (
    
      
        
          
            
              
                x
                ~
              
              I
            
            ⁡
            
              (
              t
              )
            
          
        
      
      
        
          
            
              
                x
                ~
              
              Q
            
            ⁡
            
              (
              t
              )
            
          
        
      
    
    )
  
  =
  
    
      (
      
        
          
            
              κ
              11
            
          
          
            
              κ
              12
            
          
        
        
          
            
              κ
              21
            
          
          
            
              κ
              22
            
          
        
      
      )
    
    ⁢
    
      (
      
        
          
            
              
                x
                I
              
              ⁡
              
                (
                t
                )
              
            
          
        
        
          
            
              
                x
                Q
              
              ⁡
              
                (
                t
                )
              
            
          
        
      
      )
    
  




The in-phase (I) and quadrature-phase (Q) local oscillator signals of the downconverter can be modeled as:



  
    
      LO
      I
    
    =
    
      
        (
        
          1
          +
          
            ɛ
            2
          
        
        )
      
      ⁢
      
        
      
      ⁢
      
        cos
        ⁡
        
          (
          
            
              
                ω
                c
              
              ⁢
              t
            
            +
            
              γ
              2
            
          
          )
        
      
    
  




  
    
      LO
      Q
    
    =
    
      
        (
        
          1
          +
          
            ɛ
            2
          
        
        )
      
      ⁢
      
        
      
      ⁢
      
        sin
        ⁡
        
          (
          
            
              
                ω
                c
              
              ⁢
              t
            
            +
            
              γ
              2
            
          
          )
        
      
    
  



wherein, parameters ε and γ specify the downconverter gain imbalance and phase imbalance and their impact on the local oscillators is shown in box 608.

The composite parameters in the downconverter frequency independent impairment model (described above) can be represented by:



  
    
      κ
      11
    
    =
    
      
        (
        
          1
          +
          
            ɛ
            2
          
        
        )
      
      ⁢
      
        
      
      ⁢
      
        cos
        ⁡
        
          (
          
            γ
            2
          
          )
        
      
    
  




  
    
      κ
      12
    
    =
    
      
        -
        
          (
          
            1
            +
            
              ɛ
              2
            
          
          )
        
      
      ⁢
      
        
      
      ⁢
      sin
      ⁢
      
        
      
      ⁢
      
        (
        
          γ
          2
        
        )
      
    
  




  
    
      κ
      21
    
    =
    
      
        -
        
          (
          
            1
            -
            
              ɛ
              2
            
          
          )
        
      
      ⁢
      
        
      
      ⁢
      sin
      ⁢
      
        
      
      ⁢
      
        (
        
          γ
          2
        
        )
      
    
  




  
    
      κ
      22
    
    =
    
      
        (
        
          1
          -
          
            ɛ
            2
          
        
        )
      
      ⁢
      
        
      
      ⁢
      
        cos
        ⁡
        
          (
          
            γ
            2
          
          )
        
      
    
  



The frequency dependent mismatch between the I and Q paths introduced by the downconverter and other components is modeled with hI(t) 612 and hQ(t) 610. For the purpose of this analysis, frequency dependent I, Q mismatch is ignored.
Let xε be a sparse multi-band signal received at the input to mixers 604 and 606 from filter 602. I(t) and Q(t) are the filtered outputs of the downconverter presented at the outputs of filters 612 and 610, respectively. Assume that pi(t) input to mixers 614 and 616 is a Tp periodic PRBS of length L=2L0+1, where L0ε+. Let fp=1/Tp and therefore,




  
    
      p
      i
    
    ⁡
    
      (
      t
      )
    
  
  =
  
    
      ∑
      
        n
        =
        
          -
          ∞
        
      
      ∞
    
    ⁢
    
      
        b
        
          i
          ,
          n
        
      
      ⁢
      
        e
        
          j
          ⁢
          
            
          
          ⁢
          2
          ⁢
          
            
          
          ⁢
          π
          ⁢
          
            
          
          ⁢
          
            nf
            p
          
          ⁢
          t
        
      
    
  




The weights bi,n can be evaluated by:





  
    b
    
      i
      ,
      n
    
  
  =
  
    {
    
      
        
          
            
              1
              L
            
            ⁢
            
              
                ∑
                
                  k
                  =
                  0
                
                
                  L
                  -
                  1
                
              
              ⁢
              
                β
                
                  i
                  ,
                  k
                
              
            
          
        
        
          
            
              when
              ⁢
              
                
              
              ⁢
              n
            
            =
            0
          
        
      
      
        
          
            
              ∑
              
                k
                =
                0
              
              
                L
                -
                1
              
            
            ⁢
            
              
                β
                
                  i
                  ,
                  k
                
              
              ⁢
              
                θ
                n
              
              ⁢
              
                Ψ
                
                  n
                  ,
                  k
                
              
            
          
        
        
          
            
              when
              ⁢
              
                
              
              ⁢
              n
            
            ≠
            0
          
        
      
    
  




where:

βi,0 . . . βi,L-1 are the amplitudes of the ith branch PRBS



  
    
      θ
      n
    
    =
    
      
        
          (
          
            1
            -
            
              e
              
                
                  -
                  j
                
                ⁢
                
                  
                    2
                    ⁢
                    
                      
                    
                    ⁢
                    π
                  
                  L
                
                ⁢
                n
              
            
          
          )
        
        /
        j
      
      ⁢
      
        
      
      ⁢
      2
      ⁢
      
        
      
      ⁢
      π
      ⁢
      
        
      
      ⁢
      n
    
  




  
    
      Ψ
      
        n
        ,
        k
      
    
    =
    
      e
      
        
          -
          j
        
        ⁢
        
          
            2
            ⁢
            
              
            
            ⁢
            π
          
          L
        
        ⁢
        nk
      
    
  



The Fourier transform of Ĩi(t)=Îi(t)*h(t) and {tilde over (Q)}i(t)={circumflex over (Q)}i(t)*h(t) at the outputs of filters 620 and 618, respectively, are given by:



  
    
      
        
          I
          ~
        
        i
      
      ⁡
      
        (
        f
        )
      
    
    =
    
      
        ∑
        
          n
          =
          
            -
            
              L
              0
            
          
        
        
          L
          0
        
      
      ⁢
      
        
          b
          
            i
            ,
            n
          
        
        ⁡
        
          [
          
            
              
                κ
                11
              
              ⁢
              
                
                  X
                  1
                
                ⁡
                
                  (
                  
                    f
                    -
                    
                      nf
                      p
                    
                  
                  )
                
              
            
            +
            
              
                κ
                12
              
              ⁢
              
                
                  X
                  Q
                
                ⁡
                
                  (
                  
                    f
                    -
                    
                      nf
                      p
                    
                  
                  )
                
              
            
          
          ]
        
      
    
  




  
    
      
        
          Q
          ~
        
        i
      
      ⁡
      
        (
        f
        )
      
    
    =
    
      
        ∑
        
          n
          =
          
            -
            
              L
              0
            
          
        
        
          L
          0
        
      
      ⁢
      
        
          b
          
            i
            ,
            n
          
        
        ⁡
        
          [
          
            
              
                κ
                21
              
              ⁢
              
                
                  X
                  1
                
                ⁡
                
                  (
                  
                    f
                    -
                    
                      nf
                      p
                    
                  
                  )
                
              
            
            +
            
              
                κ
                22
              
              ⁢
              
                
                  X
                  Q
                
                ⁡
                
                  (
                  
                    f
                    -
                    
                      nf
                      p
                    
                  
                  )
                
              
            
          
          ]
        
      
    
  



The inputs Îi(f) and {circumflex over (Q)}i(f) to filters 620 and 618, respectively, with impulse response h(t) are linear combinations of the fp shifted copies of I(f) and Q(f).
Since I(f), Q(f)=0 when f is not in the range −(fMAX−fMIN)/2 to (fMAX−fMIN)/2, the Fourier transforms above can be expressed with a finite sum. The signals Ĩi(t) and {tilde over (Q)}i(t) are sampled at fs samples per second. The samples yIi[n] and yQi[n] are combined and the output of the complex combine yi[n] are used to recover the support of the input signal x(t). The Fourier transform of the signals yi[n] is given by:




  
    
      Y
      i
    
    ⁡
    
      (
      
        e
        
          
            j
            ⁢
            
              
            
            ⁢
            2
            ⁢
            
              
            
            ⁢
            π
            ⁢
            
              
            
            ⁢
            
              fT
              s
            
          
          ⁢
          
            
          
        
      
      )
    
  
  =
  
    
      1
      
        T
        s
      
    
    ⁢
    
      
        ∑
        
          n
          =
          
            -
            
              L
              0
            
          
        
        
          L
          0
        
      
      ⁢
      
        
          ∑
          
            k
            =
            0
          
          
            L
            -
            1
          
        
        ⁢
        
          {
          
            
              
                β
                
                  i
                  ,
                  k
                
              
              ⁢
              
                Ψ
                
                  n
                  ,
                  k
                
              
              ⁢
              
                
                  θ
                  n
                
                ⁡
                
                  [
                  
                    
                      
                        κ
                        11
                      
                      ⁢
                      
                        
                          X
                          I
                        
                        ⁡
                        
                          (
                          
                            f
                            -
                            
                              nf
                              p
                            
                          
                          )
                        
                      
                    
                    +
                    
                      
                        κ
                        12
                      
                      ⁢
                      
                        
                          X
                          Q
                        
                        ⁡
                        
                          (
                          
                            f
                            -
                            
                              nf
                              p
                            
                          
                          )
                        
                      
                    
                  
                  ]
                
              
            
            ∓
            
              j
              ⁢
              
                
              
              ⁢
              
                β
                
                  i
                  ,
                  k
                
              
              ⁢
              
                Ψ
                
                  n
                  ,
                  k
                
              
              ⁢
              
                
                  θ
                  n
                
                ⁡
                
                  [
                  
                    
                      
                        κ
                        21
                      
                      ⁢
                      
                        
                          X
                          I
                        
                        ⁡
                        
                          (
                          
                            f
                            -
                            
                              nf
                              p
                            
                          
                          )
                        
                      
                    
                    +
                    
                      
                        κ
                        22
                      
                      ⁢
                      
                        
                          X
                          Q
                        
                        ⁡
                        
                          (
                          
                            f
                            -
                            
                              nf
                              p
                            
                          
                          )
                        
                      
                    
                  
                  ]
                
              
            
          
          }
        
      
    
  




The operation of circuit 600 can be described by:

Y(ej2πfTs)=A{tilde over (z)}(f)=Σ{tilde over (Φ)}{tilde over (Ψ)}{tilde over (θ)}K{tilde over (z)}(f)

where:

    
    
        {tilde over (Φ)}ε2m×2L is the sensing matrix (shown below);
        {tilde over (Ψ)}ε2L×2L is the dictionary matrix (shown below);
        {tilde over (θ)}ε2L×2L is a diagonal matrix (shown below) containing a set of complex weights; and
        the matrices Σ and K represent the complex combiner action and the downconverter impairments, respectively.
    
    






  
    
      Φ
      ~
    
    =
    
      [
      
        
          
            Φ
          
          
            0
          
        
        
          
            0
          
          
            Φ
          
        
      
      ]
    
  
  ;
  
    
      Ψ
      ~
    
    =
    
      [
      
        
          
            Ψ
          
          
            0
          
        
        
          
            0
          
          
            Ψ
          
        
      
      ]
    
  
  ;
  
    
      Θ
      ~
    
    =
    
      [
      
        
          
            Θ
          
          
            0
          
        
        
          
            0
          
          
            Θ
          
        
      
      ]
    
  




The complex combiner action is described by the matrix:

{tilde over (Σ)}εm×2m 

given by:





  ∑
  
    =
    
      [
      
        
          
            
              1
            
            
              ...
            
            
              0
            
          
          
            
              ⋮
            
            
              ⋱
            
            
              ⋮
            
          
          
            
              0
            
            
              ...
            
            
              1
            
          
        
        ❘
        
          
            
              
                ∓
                j
              
            
            
              ...
            
            
              0
            
          
          
            
              ⋮
            
            
              ⋱
            
            
              ⋮
            
          
          
            
              0
            
            
              ...
            
            
              
                ∓
                j
              
            
          
        
      
      ]
    
  




The block diagonal matrices

{tilde over (Ψ)}ε2m×2L 

{tilde over (Ψ)}ε2L×2L 

{tilde over (θ)}ε2L×2L 

described above include the matrices

{tilde over (Φ)}εm×L 

{tilde over (Ψ)}εL×L 

{tilde over (θ)}εL×L 

respectively.

The rows of the matrix Φ contain the amplitudes of the m unique pseudo-random bit sequences employed by the mechanisms described herein. Ψ is a discrete Fourier transform matrix and θ is a diagonal matrix containing the complex weights:




  
    θ
    n
  
  =
  
    
      
        (
        
          1
          -
          
            e
            
              
                -
                j
              
              ⁢
              
                
                  2
                  ⁢
                  
                    
                  
                  ⁢
                  π
                
                L
              
              ⁢
              n
            
          
        
        )
      
      /
      j
    
    ⁢
    
      
    
    ⁢
    2
    ⁢
    
      
    
    ⁢
    π
    ⁢
    
      
    
    ⁢
    n
  




The action of the quadrature RF downconverter with frequency independent linear impairments is described by the matrix Kε2L×2L as follows:




  κ
  =
  
    [
    
      
        
          
            κ
            11
          
        
        
          ...
        
        
          0
        
        
          
            κ
            
              1
              ,
              2
            
          
        
        
          ...
        
        
          0
        
      
      
        
          ⋮
        
        
          ⋱
        
        
          ⋮
        
        
          ⋮
        
        
          ⋱
        
        
          ⋮
        
      
      
        
          0
        
        
          ...
        
        
          
            κ
            11
          
        
        
          0
        
        
          ...
        
        
          
            κ
            12
          
        
      
      
        
          
            κ
            
              2
              ,
              1
            
          
        
        
          ...
        
        
          0
        
        
          
            κ
            22
          
        
        
          ...
        
        
          0
        
      
      
        
          ⋮
        
        
          ⋱
        
        
          ⋮
        
        
          ⋮
        
        
          ⋱
        
        
          ⋮
        
      
      
        
          0
        
        
          ...
        
        
          
            κ
            
              2
              ,
              1
            
          
        
        
          0
        
        
          ...
        
        
          
            κ
            22
          
        
      
    
    ]
  




Note that K is an identity matrix for an impairment free downconverter.

The vector {tilde over (z)}(f)ε2L in Y(ej2πfTs)=A{tilde over (z)}(f)=Σ{tilde over (Φ)}{tilde over (Ψ)}{tilde over (θ)}K{tilde over (z)}(f) includes all of the (2L0+1) frequency shifts of XI(f) and XQ(f) by fp Hz. The vector {tilde over (z)}(f) can be described as follows:




  
    
      z
      ~
    
    ⁡
    
      (
      f
      )
    
  
  ⁢
  
    (
    
      
        
          
            
              1
              2
            
            ⁡
            
              [
              
                
                  X
                  ⁡
                  
                    (
                    
                      f
                      -
                      
                        f
                        c
                      
                      +
                      
                        
                          L
                          0
                        
                        ⁢
                        
                          f
                          p
                        
                      
                    
                    )
                  
                
                +
                
                  X
                  ⁡
                  
                    (
                    
                      f
                      +
                      
                        f
                        c
                      
                      +
                      
                        
                          L
                          0
                        
                        ⁢
                        
                          f
                          p
                        
                      
                    
                    )
                  
                
              
              ]
            
          
        
      
      
        
          ⋮
        
      
      
        
          
            
              1
              2
            
            ⁡
            
              [
              
                
                  X
                  ⁡
                  
                    (
                    
                      f
                      -
                      
                        f
                        c
                      
                      -
                      
                        
                          L
                          0
                        
                        ⁢
                        
                          f
                          p
                        
                      
                    
                    )
                  
                
                +
                
                  X
                  ⁡
                  
                    (
                    
                      f
                      +
                      
                        f
                        c
                      
                      -
                      
                        
                          L
                          0
                        
                        ⁢
                        
                          f
                          p
                        
                      
                    
                    )
                  
                
              
              ]
            
          
        
      
      
        
          
            
              1
              
                2
                ⁢
                j
              
            
            ⁡
            
              [
              
                
                  X
                  ⁡
                  
                    (
                    
                      f
                      -
                      
                        f
                        c
                      
                      +
                      
                        
                          L
                          0
                        
                        ⁢
                        
                          f
                          p
                        
                      
                    
                    )
                  
                
                -
                
                  X
                  ⁡
                  
                    (
                    
                      f
                      +
                      
                        f
                        c
                      
                      +
                      
                        
                          L
                          0
                        
                        ⁢
                        
                          f
                          p
                        
                      
                    
                    )
                  
                
              
              ]
            
          
        
      
      
        
          ⋮
        
      
      
        
          
            
              1
              
                2
                ⁢
                j
              
            
            ⁡
            
              [
              
                
                  X
                  ⁡
                  
                    (
                    
                      f
                      -
                      
                        f
                        c
                      
                      -
                      
                        
                          L
                          0
                        
                        ⁢
                        
                          f
                          p
                        
                      
                    
                    )
                  
                
                -
                
                  X
                  ⁡
                  
                    (
                    
                      f
                      +
                      
                        f
                        c
                      
                      -
                      
                        
                          L
                          0
                        
                        ⁢
                        
                          f
                          p
                        
                      
                    
                    )
                  
                
              
              ]
            
          
        
      
    
    )
  




Given Y(ej2πfTs)=A{tilde over (z)}(f)=Σ{tilde over (Φ)}{tilde over (Ψ)}{tilde over (θ)}K{tilde over (z)}(f), we can attempt to recover the sparse vectors {tilde over (z)}(f) from measurements Y(f), and hence determine the frequency support of the input signal x(t). This can be done efficiently using techniques from convex optimization if the matrix A respects the geometry of the sparse vector {tilde over (z)}(f). Specifically, if for a small constant δ, the following equation holds, then the sampling and reconstruction procedure will succeed:

(1−δ)∥s∥22≦∥As∥22≦(1+δ)∥s∥22∀2K0−sparse s 

For example, if in Y(ej2πfTs)=A{tilde over (z)}(f)=Σ{tilde over (Φ)}{tilde over (Ψ)}{tilde over (θ)}K{tilde over (z)}(f), {tilde over (Φ)} is a random matrix (say with entries independent uniform ±1), the product {tilde over (Φ)}{tilde over (Ψ)} satisfies the requirement

(1−δ∥s∥22≦∥As∥22≦(1+δ)∥s∥22∀2K0−sparse s 

with high probability.

Turning to FIGS. 7-9, a time segmented QAIC is provided that implements a virtual extension of physical hardware through time segmentation and adaptive thresholding. This enables system scaling in multiple dimensions to meet user performance goals like number of detectable interferers, energy consumption and scan time, while limiting the cost and the complexity. In some embodiments, the approach can provide improved performance by virtually extending eight I/Q physical branches to sixteen I/Q through time segmentation.
In accordance with some embodiments, FIG. 7 shows an example of a rapid sensing approach exploiting compressed sampling (CS) with a time-segmented quadrature analog-to-information converter (TS-QAIC) in accordance with some embodiments. In some embodiments, this approach can deliver a 1 GHz instantaneous bandwidth (IBW) and can rapidly (<11 μs, for example) detect up to six interferers. The TS-QAIC can implement a virtual extension of physical hardware through time segmentation and adaptive thresholding, in some embodiments. This enables system scaling in multiple dimensions to meet user performance goals like number of detectable interferers, energy consumption, and scan time.
In some embodiments, the TS-QAIC maintains the advantages in power consumption and sensitivity of band pass CS approaches compared to low pass CS architectures, but it is able to detect twice the number of interferers with the same number of physical branches.
To detect six interferers, sixteen unique complex-domain measurements of the spectrum are needed.
In accordance with some embodiments, FIG. 7 shows a time-segmented rapid sensing approach in terms of a compressed sampling problem “y=Φx” (FIG. 8), where y are samples from the TS-QAIC, x is the interference with spectrum that remains stationary during slot boundaries or portions of sub-frames, and Φ is the sensing matrix constructed from two sets of unique gold sequences.
To limit silicon cost and complexity, TS-QAIC only commits eight I/Q branches on silicon and implements a virtual extension to sixteen I/Q branches through time segmentation. Assuming the spectrum is stationary for, for example, 11 μs, FIG. 8 shows how repeated application of the core hardware (eight I/Q branches) configured differently each time accomplishes virtual extension. For each successive application of the core hardware, the gold sequence generators are configured to generate a different set of eight unique sequences gj/k(t).
The 2.7-3.7 GHz TS-QAIC front-end chip (FIG. 9) employs a wideband current-reuse noise-canceling low-noise amplifier (e.g., 5.7 mW) and a wideband programmable bandwidth (e.g., BW settings of 125 MHz, 250 MHz, and 500 MHz) RF I/Q downconverter (18.37 mW incl. LO I/Q div. by 2). The RF I/Q downconverter is followed by eight I/Q baseband PN mixing branches (36.88 mW) that are driven by two sets of eight unique gold sequences. Baseband low pass filtering is performed with a transimpedance amplifier which is implemented as a two-stage operational transconductance amplifier with Miller compensation, and 20 MSps ADCs sample the branches; a pairwise complex combiner is used prior to complex-domain CS support recovery to identify the locations of six interferers. The on-chip gold sequence generator (6.68 mW) has a programmable set/reset option for two six flip-flop LFSRs to generate unique sequences based on the initial word settings. It generates six 63-long gold sequences by XORing two m-sequences generated by two six-flip-flop LFSRs operating at 1.26 GHz. For a 20 MHz resolution bandwidth (RBW), the eight PN I/Q mixing stages are driven by six time segmented 63-long gold sequences and two time-segmented 63-long m-sequences with sufficiently low cross correlation and low mutual coherence in the CS sensing matrix.
For experimental validation of the TS-QAIC, multi-band RF signals with up to six (10 MHz wide upconverted filtered noise) bands are generated and fed into the chip. Gold sequences with low mutual coherence are selected and the outputs are digitized and stored for off-line CS DSP complex-domain support recovery with the CS orthogonal matching pursuit algorithm. FIG. 10 illustrates how to select gold sequence sets for optimal detection probability (PD) and false alarm probability (PFA) performance of the TS-QAIC. The measured PD and PFA for varying power levels per band for six interferers is shown when two sensing matrices with different properties each constructed from two time-segmented gold sequence sets are used. The measured PD is >90% for signals with a power level larger than −70 dBm/10 MHz when the optimal sensing matrix is selected, while the sub-optimal sensing matrix cannot deliver a PD>90%. The optimal sensing matrix has a lower average and a lower maximum mutual coherence which is needed for successful CS support recovery (FIG. 11).
FIG. 11 illustrates an example 1100 of hardware that can be used to implement one or more of support recovery block 158, signal reconstruction block 160, and system control and user interface 162. In some of more embodiments, two or more of support recovery block 158, signal reconstruction block 160, and system control and user interface 162 can be implemented in the same or different hardware 1100.
As shown in FIG. 11, hardware 1100 can include a hardware processor 1102, memory/storage 1104, an input interface 1106, an output interface 1108, and/or any other suitable components, which can be interconnected. Hardware 1100 can be implemented in some embodiments as any of a general purpose device (such as a computer) or a special purpose device (such as a client, a server, etc.).
Hardware processor 1102 can be any suitable hardware device for performing the functions associated with support recovery block 158, signal reconstruction block 160, system control and user interface 162, and/or any other component described herein, such as a microprocessor, a digital signal processor, a controller, etc., in some embodiments. For example, hardware processor 1102 can execute instructions stored in memory/storage 1104 for performing such functions.
In some embodiments, memory/storage 1104 can be any suitable memory and/or storage, such as random access memory, read only memory, programmable read only memory, flash memory, a hard disk, a solid state drive, non-transitory computer-readable media, etc. This memory/storage can store any suitable instructions, programs, data, information, etc.
Input interface 1106 can be any suitable interface for receiving data, programs, and/or any other suitable digital information.
Output interface 1108 can be any suitable interface for transmitting and/or presenting (e.g., via audio, video, etc.) data, programs, and/or any other suitable digital information.
In some embodiments, any suitable computer readable media can be used for storing instructions for performing the functions and/or processes described herein. Such computer readable media can be part of, or separate from, storage/memory 1104. For example, in some embodiments, computer readable media can be transitory or non-transitory. For example, non-transitory computer readable media can include media such as magnetic media (such as hard disks, floppy disks, etc.), optical media (such as compact discs, digital video discs, Blu-ray discs, etc.), semiconductor media (such as random access memory (RAM), flash memory, electrically programmable read only memory (EPROM), electrically erasable programmable read only memory (EEPROM), etc.), any suitable media that is not fleeting or devoid of any semblance of permanence during transmission, and/or any suitable tangible media. As another example, transitory computer readable media can include signals on networks, in wires, conductors, optical fibers, circuits, any suitable media that is fleeting and devoid of any semblance of permanence during transmission, and/or any suitable intangible media.
The provision of the examples described herein (as well as clauses phrased as “such as,” “e.g.,” “including,” and the like) should not be interpreted as limiting the claimed subject matter to the specific examples; rather, the examples are intended to illustrate only some of many possible aspects. It should also be noted that, as used herein, the term mechanism can encompass hardware, software, firmware, or any suitable combination thereof.
Accordingly, mechanisms (which can include circuits, systems, methods, and computer readable media) for detecting interferers in a frequency range are provided.
Although the invention has been described and illustrated in the foregoing illustrative embodiments, it is understood that the present disclosure has been made only by way of example, and that numerous changes in the details of implementation of the invention can be made without departing from the spirit and scope of the invention, which is limited only by the claims that follow. Features of the disclosed embodiments can be combined and rearranged in various ways.

## Claims

1. A circuit for detecting interferers, comprising:
a first in-phase mixer that receives and mixes a radio frequency (RF) signal and an in-phase local oscillator signal to produce a first in-phase mixer output signal;
a first quadrature-phase mixer that receives and mixes the radio frequency (RF) signal and a quadrature-phase local oscillator signal to produce a first quadrature-phase mixer output signal;
a first in-phase filter that receives and filters the first in-phase mixer output signal and produces a first in-phase filtered signal;
a first quadrature-phase filter that receives and filters the first quadrature-phase mixer output signal and produces a first quadrature-phase filtered signal;
a first in-phase branch that comprises:
a second in-phase mixer that receives and mixes the first in-phase filtered signal and a first pseudorandom noise signal to produce a second in-phase mixer output signal;
a second in-phase filter that receives and filters the second in-phase mixer output signal to produce a second in-phase filtered signal; and
a first in-phase analog-to-digital converter that receives the second in-phase filtered signal and produces a first in-phase digitized signal;

a second in-phase branch that comprises:
a third in-phase mixer that receives and mixes the first in-phase filtered signal and a second pseudorandom noise signal to produce a third in-phase mixer output signal;
a third in-phase filter that receives and filters the third in-phase mixer output signal to produce a third in-phase filtered signal; and
a second in-phase analog-to-digital converter that receives the third in-phase filtered signal and produces a second in-phase digitized signal;

a first quadrature-phase branch that comprises:
a second quadrature-phase mixer that receives and mixes the first quadrature-phase filtered signal and the first pseudorandom noise signal to produce a second quadrature-phase mixer output signal;
a second quadrature-phase filter that receives and filters the second quadrature-phase mixer output signal to produce a second quadrature-phase filtered signal; and
a first quadrature-phase analog-to-digital converter that receives the second quadrature-phase filtered signal and produces a first quadrature-phase digitized signal; and

a second quadrature-phase branch that comprises:
a third quadrature-phase mixer that receives and mixes the first quadrature-phase filtered signal and the second pseudorandom noise signal to produce a third quadrature-phase mixer output signal;
a third quadrature-phase filter that receives and filters the third quadrature-phase mixer output signal to produce a third quadrature-phase filtered signal; and
a second quadrature-phase analog-to-digital converter that receives the third quadrature-phase filtered signal and produces a second quadrature-phase digitized signal;

a complex combiner that combines the first in-phase digitized signal and the first quadrature-phase digitized signal to produce a first combined signal and that combines the second in-phase digitized signal and the second quadrature-phase digitized signal to produce a second combined signal; and
at least one hardware processor that receives the first combined signal and the second combined signal and that identifies at least one interferer in the RF signal using the first combined signal and the second combined signal using an orthogonal matching pursuit technique.

2. The circuit of claim 1, further comprising a low noise amplifier that outputs the RF signal.

3. The circuit of claim 1, wherein the quadrature-phase local oscillator signal is shifted 90 degrees from the in-phase local oscillator.

4. The circuit of claim 1, wherein the first pseudorandom noise signal and the second pseudorandom noise signal are Gold sequences.

5. The circuit of claim 4, further comprising a Gold sequence generator.

6. The circuit of claim 1, wherein the at least one hardware processor also determines an estimate of an input signal represented by the RF signal using the first combined signal and the second combined signal.

7. The circuit of claim 1, wherein the complex combiner: combines the first in-phase digitized signal (XBase-Band-in-Phase1) and the first quadrature-phase digitized signal (XBase-Band-Quadrature1) to produce the first combined signal (y1), wherein y1=XBase-Band-In-Phase1∓jXBase-Band-Quadrature1; and that combines the second in-phase digitized signal (XBase-Band-In-Phase2) and the second quadrature-phase digitized signal (XBase-Band-Quadrature2) to produce a second combined signal (y2), wherein y2=XBase-Band-In-Phase2∓jXBase-Band-Quadrature2.

8. A method for detecting interferers, comprising:
mixing a radio frequency (RF) signal and an in-phase local oscillator signal to produce a first in-phase mixer output signal;
mixing the radio frequency (RF) signal and a quadrature-phase local oscillator signal to produce a first quadrature-phase mixer output signal;
filtering the first in-phase mixer output signal to produce a first in-phase filtered signal;
filtering the first quadrature-phase mixer output signal to produce a first quadrature-phase filtered signal;
mixing the first in-phase filtered signal and a first pseudorandom noise signal to produce a second in-phase mixer output signal;
filtering the second in-phase mixer output signal to produce a second in-phase filtered signal;
analog-to-digital converting the second in-phase filtered signal to produce a first in-phase digitized signal;
mixing the first in-phase filtered signal and a second pseudorandom noise signal to produce a third in-phase mixer output signal;
filtering the third in-phase mixer output signal to produce a third in-phase filtered signal;
analog-to-digital converting the third in-phase filtered signal to produce a second in-phase digitized signal;
mixing the first quadrature-phase filtered signal and the first pseudorandom noise signal to produce a second quadrature-phase mixer output signal;
filtering the second quadrature-phase mixer output signal to produce a second quadrature-phase filtered signal;
analog-to-digital converting the second quadrature-phase filtered signal to produce a first quadrature-phase digitized signal;
mixing the first quadrature-phase filtered signal and the second pseudorandom noise signal to produce a third quadrature-phase mixer output signal;
filtering the third quadrature-phase mixer output signal to produce a third quadrature-phase filtered signal;
analog-to-digital converting the third quadrature-phase filtered signal to produce a second quadrature-phase digitized signal;
combining the first in-phase digitized signal and the first quadrature-phase digitized signal to produce a first combined signal and combining the second in-phase digitized signal and the second quadrature-phase digitized signal to produce a second combined signal; and
identifying at least one interferer in the RF signal using the first combined signal and the second combined signal using an orthogonal matching pursuit technique.

9. The method of claim 8, further comprising amplifying an input signal to produce the RF signal using a low noise amplifier.

10. The method of claim 8, wherein the quadrature-phase local oscillator signal is shifted 90 degrees from the in-phase local oscillator.

11. The method of claim 8, wherein the first pseudorandom noise signal and the second pseudorandom noise signal are Gold sequences.

12. The method of claim 11, further comprising generating the Gold sequences using a Gold sequence generator.

13. The method of claim 8, further comprising determining an estimate of an input signal represented by the RF signal using the first combined signal and the second combined signal.

14. The method of claim 8, wherein: combining the first in-phase digitized signal (XBase-Band-In-Phase1) and the first quadrature-phase digitized signal (XBase-Band-Quadrature1) to produce the first combined signal (y1), wherein y1=XBase-Band-In-Phase1∓jXBase-Band-Quadrature1; and combining the second in-phase digitized signal (XBase-Band-In-Phase2) and the second quadrature-phase digitized signal (XBase-Band-Quadrature2) to produce a second combined signal (y2), wherein y2=XBase-Band-In-Phase2∓jXBase-Band-Quadrature2.