U.S. patent application number 16/683103 was filed with the patent office on 2020-06-18 for methods for operating stepped frequency radar systems with feedback based step size zoom.
The applicant listed for this patent is MOVANO INC.. Invention is credited to Michael A. LEABMAN.
Application Number | 20200191944 16/683103 |
Document ID | / |
Family ID | 71073509 |
Filed Date | 2020-06-18 |
![](/patent/app/20200191944/US20200191944A1-20200618-D00000.png)
![](/patent/app/20200191944/US20200191944A1-20200618-D00001.png)
![](/patent/app/20200191944/US20200191944A1-20200618-D00002.png)
![](/patent/app/20200191944/US20200191944A1-20200618-D00003.png)
![](/patent/app/20200191944/US20200191944A1-20200618-D00004.png)
![](/patent/app/20200191944/US20200191944A1-20200618-D00005.png)
![](/patent/app/20200191944/US20200191944A1-20200618-D00006.png)
![](/patent/app/20200191944/US20200191944A1-20200618-D00007.png)
![](/patent/app/20200191944/US20200191944A1-20200618-D00008.png)
![](/patent/app/20200191944/US20200191944A1-20200618-D00009.png)
![](/patent/app/20200191944/US20200191944A1-20200618-D00010.png)
View All Diagrams
United States Patent
Application |
20200191944 |
Kind Code |
A1 |
LEABMAN; Michael A. |
June 18, 2020 |
METHODS FOR OPERATING STEPPED FREQUENCY RADAR SYSTEMS WITH FEEDBACK
BASED STEP SIZE ZOOM
Abstract
A method for operating a stepped frequency radar system is
disclosed. The method involves performing stepped frequency
scanning across a first frequency range using frequency steps of a
first step size, the stepped frequency scanning performed using at
least one transmit antenna and a two-dimensional array of receive
antennas, evaluating data generated from the stepped frequency
scanning across the first frequency range, changing from the first
step size to a second step size in response to the data evaluation,
wherein the second step size is different from the first step size,
and performing stepped frequency scanning across a second frequency
range using the at least one transmit antenna and the
two-dimensional array of receive antennas and using frequency steps
of the second step size.
Inventors: |
LEABMAN; Michael A.; (San
Ramon, CA) |
|
Applicant: |
Name |
City |
State |
Country |
Type |
MOVANO INC. |
San Ramon |
CA |
US |
|
|
Family ID: |
71073509 |
Appl. No.: |
16/683103 |
Filed: |
November 13, 2019 |
Related U.S. Patent Documents
|
|
|
|
|
|
Application
Number |
Filing Date |
Patent Number |
|
|
62781523 |
Dec 18, 2018 |
|
|
|
62886642 |
Aug 14, 2019 |
|
|
|
Current U.S.
Class: |
1/1 |
Current CPC
Class: |
G01S 13/26 20130101;
G01S 13/76 20130101; G01S 7/34 20130101; G01S 13/32 20130101; G01S
7/35 20130101; G01S 13/0209 20130101 |
International
Class: |
G01S 13/76 20060101
G01S013/76; G01S 13/32 20060101 G01S013/32 |
Claims
1. A method for operating a stepped frequency radar system, the
method comprising: performing stepped frequency scanning across a
first frequency range using frequency steps of a first step size,
the stepped frequency scanning performed using at least one
transmit antenna and a two-dimensional array of receive antennas;
evaluating data generated from the stepped frequency scanning
across the first frequency range; and changing from the first step
size to a second step size in response to the data evaluation,
wherein the second step size is different from the first step size;
and performing stepped frequency scanning across a second frequency
range using the at least one transmit antenna and the
two-dimensional array of receive antennas and using frequency steps
of the second step size.
2. The method of claim 1, wherein the frequency step size is
changed from the first step size to the second step size in
accordance with a digital frequency control signal.
3. The method of claim 1, wherein the second step size is smaller
than the first step size.
4. The method of claim 1, wherein the first frequency range and the
second frequency range are in the range of 2-6 GHz.
5. The method of claim 1, further comprising: evaluating data
generated from the stepped frequency scanning across the second
frequency range; changing from the second step size to a third step
size in response to the data evaluation, wherein the third step
size is different from the second step size; and performing stepped
frequency scanning across the third frequency range using the at
least one transmit antenna and the two-dimensional array of receive
antennas and using frequency steps of the second step size and
using frequency steps of a third step size.
6. The method of claim 5, wherein the third step size is smaller
than the second step size.
7. The method of claim 1, wherein evaluating data generated from
the stepped frequency scanning across the first frequency range
comprises identifying an increase in magnitude of received RF
energy at wavelengths that correspond to known resonant resonant
wavelengths of a weapon.
Description
BACKGROUND
[0001] Radar detection involves transmitting electromagnetic energy
and receiving reflected portions of the transmitted electromagnetic
energy. Techniques for transmitting electromagnetic energy in radar
systems include impulse, chirp, and stepped frequency techniques.
Stepped frequency radar has traditionally been implemented by
repeatedly scanning over the same frequency range using the same
step size. For example, a frequency burst of stepped frequency
pulses over the same frequency range with the same step size and
the same number of steps is continuously repeated to implement
stepped frequency radar. Although traditional stepped frequency
radar works well, there is a need to expand the capabilities of
stepped frequency radar.
SUMMARY
[0002] A method for operating a stepped frequency radar system is
disclosed. The method involves performing stepped frequency
scanning across a first frequency range using frequency steps of a
first step size, the stepped frequency scanning performed using at
least one transmit antenna and a two- dimensional array of receive
antennas, evaluating data generated from the stepped frequency
scanning across the first frequency range, changing from the first
step size to a second step size in response to the data evaluation,
wherein the second step size is different from the first step size,
and performing stepped frequency scanning across a second frequency
range using the at least one transmit antenna and the
two-dimensional array of receive antennas and using frequency steps
of the second step size.
[0003] Other aspects in accordance with the invention will become
apparent from the following detailed description, taken in
conjunction with the accompanying drawings, illustrated by way of
example of the principles of the invention.
BRIEF DESCRIPTION OF THE DRAWINGS
[0004] FIGS. 1A-1C depict frequency versus time graphs of impulse,
chirp, and stepped frequency techniques for transmitting
electromagnetic energy in a radar system.
[0005] FIG. 2 depicts a burst of electromagnetic energy using
stepped frequency transmission.
[0006] FIG. 3A depicts a graph of the transmission bandwidth, B, of
transmitted electromagnetic energy in the frequency range of 2-6
GHz.
[0007] FIG. 3B depicts a graph of stepped frequency pulses that
have a repetition interval, T, and a step size, .DELTA.f, of 62.5
MHz.
[0008] FIG. 4A depicts a frequency versus time graph of
transmission pulses, with transmit (TX) interval and receive (RX)
intervals identified relative to the pulses.
[0009] FIG. 4B depicts an amplitude versus time graph of the
transmission waveforms that corresponds to FIG. 16A.
[0010] FIG. 5 illustrates operations related to transmitting,
receiving, and processing phases of the sensor system
operation.
[0011] FIG. 6 depicts a functional block diagram of an embodiment
of a sensor system that utilizes millimeter range radio waves.
[0012] FIG. 7 depicts an expanded view of an embodiment of portions
of the sensor system of FIG. 6, including elements of the RF
front-end.
[0013] FIG. 8 depicts an embodiment of the IF/BB component shown in
FIG. 7.
[0014] FIG. 9 illustrates the frequency range of 2-6 GHz relative
to different range scales.
[0015] FIG. 10 depicts the frequency range of 2-6 GHz relative to a
range scale of 256.
[0016] FIG. 11 is a process flow diagram of operation of stepped
frequency radar scanning.
[0017] FIG. 12 depicts a feedback loop between the transmit and
receive elements of the sensor system described with reference to
FIGS. 6 and 7.
[0018] FIGS. 13A and 13B illustrate two different examples of a
scanning operation, which involves scanning a relatively wide
frequency range at a first step size and scanning a more narrow
frequency range at a smaller step size or step sizes.
[0019] FIGS. 14A and 14B illustrate digital frequency control
signals that correspond to the stepped frequency scanning
operations illustrated in FIGS. 13A and 13B, respectively.
[0020] FIG. 15A illustrates an example of frequency hopping in a
stepped frequency scanning operation.
[0021] FIG. 15B illustrates digital frequency control signals that
correspond to the frequency hopping operation illustrated in FIG.
15A.
[0022] FIG. 16 illustrates an example of a case in which frequency
hopping is implemented in stepped frequency radar to avoid
frequency bands of known interference.
[0023] FIG. 17 illustrates a process in which a frequency range is
first scanned to identify an interfering frequency band and then
the subsequent scan is controlled to hop over the identified
interfering frequency band.
[0024] FIG. 18A illustrates stepped frequency scanning over the 2-6
GHz frequency range in which ranging scanning is performed over the
entire 2-6 GHz frequency range simultaneously with imaging scanning
that is performed over only the 4-5 GHz frequency range.
[0025] FIG. 18B illustrates digital frequency coding for the
stepped frequency scanning illustrated in FIG. 18A.
[0026] FIG. 18C illustrates another example of digital frequency
coding for the stepped frequency scanning illustrated in FIG.
18A.
[0027] FIG. 19A depicts an area that includes two sensor systems,
such as the sensor systems described with reference to FIGS. 6-8,
which may interfere with each other.
[0028] FIG. 19B illustrates encoding and corresponding decoding of
discrete frequency pulses transmitted from the two sensor systems
depicted in FIG. 19A.
[0029] FIG. 20 depicts an expanded view of an embodiment of
portions of the sensor system of FIG. 6, including elements of the
RF front-end.
[0030] FIG. 21A depicts and embodiment of a 2.times.2 array of
sensor systems such as the sensors systems described with reference
to FIGS. 6-8.
[0031] FIG. 21B illustrates an example of transmission frequency
diversity that can be implemented by the sensor array of FIG.
23A.
[0032] FIG. 22 is an embodiment of a DSP that includes a ranging
component and an imaging component.
[0033] Throughout the description, similar reference numbers may be
used to identify similar elements.
DETAILED DESCRIPTION
[0034] It will be readily understood that the components of the
embodiments as generally described herein and illustrated in the
appended figures could be arranged and designed in a wide variety
of different configurations. Thus, the following more detailed
description of various embodiments, as represented in the figures,
is not intended to limit the scope of the present disclosure, but
is merely representative of various embodiments. While the various
aspects of the embodiments are presented in drawings, the drawings
are not necessarily drawn to scale unless specifically
indicated.
[0035] The present invention may be embodied in other specific
forms without departing from its spirit or essential
characteristics. The described embodiments are to be considered in
all respects only as illustrative and not restrictive. The scope of
the invention is, therefore, indicated by the appended claims
rather than by this detailed description. All changes which come
within the meaning and range of equivalency of the claims are to be
embraced within their scope.
[0036] Reference throughout this specification to features,
advantages, or similar language does not imply that all of the
features and advantages that may be realized with the present
invention should be or are in any single embodiment of the
invention. Rather, language referring to the features and
advantages is understood to mean that a specific feature,
advantage, or characteristic described in connection with an
embodiment is included in at least one embodiment of the present
invention. Thus, discussions of the features and advantages, and
similar language, throughout this specification may, but do not
necessarily, refer to the same embodiment.
[0037] Furthermore, the described features, advantages, and
characteristics of the invention may be combined in any suitable
manner in one or more embodiments. One skilled in the relevant art
will recognize, in light of the description herein, that the
invention can be practiced without one or more of the specific
features or advantages of a particular embodiment. In other
instances, additional features and advantages may be recognized in
certain embodiments that may not be present in all embodiments of
the invention.
[0038] Reference throughout this specification to "one embodiment",
"an embodiment", or similar language means that a particular
feature, structure, or characteristic described in connection with
the indicated embodiment is included in at least one embodiment of
the present invention. Thus, the phrases "in one embodiment", "in
an embodiment", and similar language throughout this specification
may, but do not necessarily, all refer to the same embodiment.
[0039] As is known in the field, radar detection involves
transmitting electromagnetic energy and receiving reflected
portions of the transmitted electromagnetic energy. Techniques for
transmitting electromagnetic energy in radar systems include
impulse, chirp, and stepped frequency techniques.
[0040] FIGS. 1A-1C depict frequency versus time graphs of impulse,
chirp, and stepped frequency techniques for transmitting
electromagnetic energy in a radar system. FIG. 1A depicts a radar
transmission technique that involves transmitting pulses of
electromagnetic energy at the same frequency for each pulse,
referred to as "impulse" transmission. In the example of FIG. 1A,
each pulse is at frequency, f.sub.1, and lasts for a constant
interval of approximately 2 ns. The pulses are each separated by
approximately 2 ns.
[0041] FIG. 1B depicts a radar transmission technique that involves
transmitting pulses of electromagnetic energy at an increasing
frequency for each interval, referred to herein as "chirp"
transmission. In the example of FIG. 1B, each chirp increases in
frequency from frequency f.sub.0 to f.sub.1 over an interval of 2
ns and each chirp is separated by 2 ns. In other embodiments, the
chirps may be separated by very short intervals (e.g., a fraction
of a nanosecond) or no interval.
[0042] FIG. 1C depicts a radar transmission technique that involves
transmitting pulses of electromagnetic energy at the same frequency
during a particular pulse but at an increased frequency from
pulse-to-pulse, referred to herein as a "stepped frequency"
transmission or a stepped frequency pattern. In the example of FIG.
1C, each pulse has a constant frequency over the interval of the
pulse (e.g., over 2 ns), but the frequency increases by an
increment of .DELTA.f (referred to as a "step size") from
pulse-to-pulse. For example, the frequency of the first pulse is
f.sub.0, the frequency of the second pulse is f.sub.0+.DELTA.f, the
frequency of the third pulse is f.sub.0+2 .DELTA.f, and the
frequency of the fourth pulse is f.sub.0+3 .DELTA.f, and so on.
[0043] In an embodiment, the sensor system described herein is
operated using stepped frequency transmissions to implement stepped
frequency scanning. Operation of the sensor system using stepped
frequency transmissions to implement stepped frequency scanning is
described in more detail below. FIG. 2 depicts a burst of
electromagnetic energy over a frequency range that includes
multiple steps using stepped frequency transmission. The frequency
of the pulses in the multi-step burst can be expressed as:
f.sub.n=f.sub.0+n.DELTA.f
where f.sub.0=starting carrier frequency, .DELTA.f=step size,
.tau.=pulse length (active, per frequency), T=repetition interval,
n=1, . . . N, each burst consists of N pulses (frequencies) and a
coherent processing interval (CPI)=NT=1 full burst. In an
embodiment, the repetition interval corresponds to the sweep rate
of the stepped frequency scanning and the width of the full burst
is referred to as the frequency range or the stepped frequency
scanning range.
[0044] Using stepped frequency scanning enables relatively high
range resolution. High range resolution can be advantageous in
ranging and 3D radar imaging, which can have applications such as
identifying objects, e.g., a weapon on a person that may, for
example, be made of a reflective material and that may have a size
in the range of 25 cm.times.12 cm, e.g., the size of a typical
handgun. In an embodiment, in order to effectively isolate a signal
that corresponds to reflections of electromagnetic energy from an
object such as a hand-held weapon, it is desirable to have a
corresponding range resolution, which may be provided by the 2-6
GHz frequency range.
[0045] Using stepped frequency scanning, range resolution can be
expressed as:
.DELTA.R=c/2B
wherein c=speed of light, B=effective bandwidth. The range
resolution can then be expressed as:
.DELTA.R=c/2N.DELTA.f
wherein B=N.DELTA.f. Thus, range resolution does not depend on
instantaneous bandwidth and the range resolution can be increased
arbitrarily by increasing N.DELTA.f.
[0046] In an embodiment, electromagnetic energy is transmitted from
at least one antenna (referred to as a "TX antenna") of a stepped
frequency radar system in the frequency range of approximately 2-6
GHz, which corresponds to a total bandwidth of approximately 4 GHz,
e.g., B =4 GHz. FIG. 3A depicts a graph of the transmission
bandwidth, B, of transmitted electromagnetic energy in the
frequency range of 2-6 GHz. Within a 4 GHz bandwidth, from 2-6 GHz,
discrete frequencies (e.g., frequency pulses each centered at a
different frequency) can be transmitted. For example, in an
embodiment, the number of discrete frequencies that can be
transmitted ranges from, for example, 64-1,024 discrete
frequencies, e.g., 64, 128, 256, 512, or 1,024 discrete
frequencies. In a case in which 64 discrete frequencies are
available and a repetition interval, T, over 4 GHz of bandwidth,
the step size, .DELTA.f, is 62.5 MHz (e.g., 4 GHz of bandwidth
divided by 64 =62.5 MHz) and in a case with 256 discrete
frequencies available and a repetition interval, T, over 4 GHz of
bandwidth, the step size, .DELTA.f, is 15.625 MHz (e.g., 4 GHz of
bandwidth divided by 256=15.625 MHz).
[0047] FIG. 3B depicts a graph of stepped frequency pulses that
have a repetition interval, T, and a step size, .DELTA.f, of 62.5
MHz (e.g., 4 GHz of bandwidth divided by 64=62.5 MHz). As is
described below, an example sensor system may have two TX antennas
and four receive (RX) antennas. Assuming a discrete frequency can
be received on each RX antenna, degrees of freedom (DOF) of the
sensor system in the receive operations can be expressed as: 4 RX
antennas.times.64 discrete frequencies=256 DOF; and 4 RX
antennas.times.256 discrete frequencies=1K DOF. The number of
degrees of freedom (also referred to as "transmission frequency
diversity") can provide signal diversity, which can be beneficial
in 3D radar imaging. For example, the different discrete
frequencies may have different responses to different objects,
e.g., different types of weapons. Thus, greater transmission
frequency diversity can translate to greater signal diversity, and
ultimately to more accurate 3D radar imaging.
[0048] One feature of stepped frequency radar is that the sensor
system receives reflected electromagnetic energy at basically the
same frequency over the repetition interval, T. That is, as opposed
to chirp transmission, the frequency of the pulse does not change
over the interval of the pulse and therefore the received reflected
electromagnetic energy is at the same frequency as the transmitted
electromagnetic energy for the respective interval. FIG. 4A depicts
stepped frequency scanning as a frequency versus time graph of
transmission pulses, with transmit (TX) and receive (RX) intervals
identified relative to the pulses. As illustrated in FIG. 4A, RX
operations for the first pulse occur during the pulse length,
.tau., of repetition interval, T, and during the interval between
the next pulse. FIG. 4B depicts an amplitude versus time graph of
the transmission waveforms that corresponds to FIG. 4A. As
illustrated in FIG. 4B, the amplitude of the pulses is constant
while the frequency increases by .DELTA.f at each repetition
interval, T.
[0049] In an embodiment, the power of the transmitted
electromagnetic energy can be set to achieve a desired transmission
distance and/or a desired. In an embodiment, the transmission power
from the TX antennas is about 20 dBm.
[0050] In an embodiment, electromagnetic energy can be transmitted
from the TX antennas one TX antenna at a time (referred to herein
as "transmit diversity"). For example, a signal is transmitted from
a first one of two TX antennas while the second one of the two TX
antennas is idle and then a signal is transmitted from the second
TX antenna while the first TX antenna is idle. Transmit diversity
may reveal that illumination from one of the two TX antennas
provides a higher quality signal than illumination from the other
of two TX antennas. This may be especially true when trying to
identify an object such as a person or a weapon carried by a
person. Thus, transmit diversity can provide sets of received
signals that are independent of each other and may have different
characteristics, e.g., signal power, SNR, etc.
[0051] Some theory related to operating a stepped frequency radar
system to implement stepped frequency scanning is described with
reference to FIG. 5, which illustrates operations related to
transmitting, receiving, and processing phases of a sensor system
operation. With reference to the upper portion of FIG. 5, a time
versus amplitude graph of a transmitted signal burst, similar to
the graph of FIG. 4B, is shown. The graph represents the waveforms
of five pulses of a burst at frequencies of f.sub.0,
f.sub.0+.DELTA.f, f.sub.0+2.DELTA., f.sub.0+3.DELTA.f, and
f.sub.0+4.DELTA.f.
[0052] The middle portion of FIG. 5 represents values of received
signals that correspond to the amplitude, phase, and frequency of
each pulse in the burst of four pulses. In an embodiment, received
signals are placed in range bins such that there is one complex
sample per range bin per frequency. Inverse Discrete Fourier
Transforms (IDFTs) are then performed on a per-range bin basis to
determine range information. The bottom portion of FIG. 5
illustrates an IDFT process that produces a signal that corresponds
to the range of a particular object. For example, the range may
correspond to an object such as a person or a weapon carried by a
person. In stepped frequency radar, the process of transmitting the
frequency pulses in bursts of N pulses is repeated over the same
frequency range to determine the range of object. Additionally, the
process can be repeated using a 2D array of receive antennas to
obtain 2D information that can be used for 2D and/or 3D imaging. In
an embodiment, some portion of the signal processing is performed
digitally by a DSP or CPU. Although one example of a signal
processing scheme is described with reference to FIG. 5, other
signal processing schemes may be implemented to isolate signals
that correspond to reflections from objects of interest from
signals that correspond to reflections from other undesired objects
and from signals that correspond to leakage from the TX
antennas.
[0053] As described above with reference to FIGS. 1C-5, stepped
frequency radar scanning is typically implemented by repeatedly
scanning over the same frequency range (e.g., one full burst) with
multiple RF pulses that increase in frequency by the same step
size. For example, with reference to FIGS. 3B, 4A, and 4B, a
frequency burst of stepped frequency pulses over the same frequency
range with the same step size and the same number of steps is
repeatedly transmitted to implement stepped frequency scanning.
However, it has been realized that digital control of discrete
frequencies in a stepped frequency radar system enables approaches
to stepped frequency RF scanning and applications for stepped
frequency radar that heretofore have not been envisioned. For
example, digital control of discrete frequencies in a stepped
frequency radar system enables the step size, frequency range,
and/or discrete frequencies to be changed during a stepped
frequency scanning operation in various unique ways. In an
embodiment, the step size can be changed to a smaller step size to,
for example, provide greater imaging resolution within a particular
frequency band of interest. In some instances, the step size can be
changed "on-the-fly" in response to feedback from the stepped
frequency scanning and in other instances a change in step size can
be preprogrammed. In another embodiment, the scanned frequency
range can be changed to avoid, or "hop" over, a frequency band that
may interfere with the scanning operation. Frequency hopping may be
implemented to, for example, avoid frequency bands that are known
to cause interference and/or frequency hopping may be adapted to
avoid interfering frequency bands that are learned by the system.
In another embodiment, simultaneous stepped frequency scanning for
ranging and stepped frequency scanning for imaging (e.g., 2D or 3D
imaging) can be accomplished by selectively associating digital
scanning data with different ranging and imaging data buckets for
digital processing. In another embodiment, interference between two
stepped frequency radar systems can be mitigated by encoding the
discrete frequencies of the stepped frequency scanning (e.g., in a
pseudorandom manner) so that frequency pulses at the same frequency
are unlikely to be transmitted by two stepped frequency radar
systems at the same time. As is described below, digital control of
discrete frequencies in a stepped frequency radar system provides
spectral agility that can be utilized to implement approaches to
stepped frequency scanning and applications for stepped frequency
radar that heretofore have not been envisioned.
[0054] FIG. 6 depicts a functional block diagram of an embodiment
of a sensor system 610 that utilizes millimeter range radio waves
to implement stepped frequency radar to implement operations such
as ranging and imaging, including 2D or 3D imaging. The sensor
system includes transmit (TX) antennas 644, receive (RX) antennas
646, an RF front-end 648, a digital baseband system 650, and a CPU
652. The components of the sensor system may be integrated together
in various ways. For example, some combination of components may be
fabricated on the same semiconductor substrate and/or included in
the same packaged IC device or a combination of packaged IC
devices. In an embodiment, the sensor system is designed to
transmit and receive radio waves in the range of 2-6 GHz and/or in
the range of 122-126 GHz. The sensor system may also operate in
other frequency ranges, such as in a range around 24 GHz and/or in
a range around 60 GHz,
[0055] In the embodiment of FIG. 6, the sensor system 610 includes
two TX antennas 544 and four RX antennas 646. Although two TX and
four RX antennas are used, there could be another number of
antennas, e.g., one or more TX antennas and three or more RX
antennas. In an embodiment, the RX antennas are configured in a 2D
array. In an embodiment, the TX and RX antennas are configured to
transmit and receive radio waves, respectively. For example, the
antennas are configured to transmit and receive radio waves in the
2-6 GHz frequency range, e.g., wavelengths in the range of
149.89-49.96 mm and/or in the 122-126 GHz frequency range, e.g.,
wavelengths in the range of 2.46-2.38 mm.
[0056] In the embodiment of FIG. 6, the RF front-end 648 includes a
transmit (TX) component 654, a receive (RX) component 656, a
frequency synthesizer 658, and an analogue processing component
660. The transmit component may include elements such as power
amplifiers (PAs) and mixers. The receive component may include
elements such as low noise amplifiers (LNAs), variable gain
amplifiers (VGAs), and mixers. The frequency synthesizer includes
elements to generate electrical signals at frequencies that are
used by the transmit and receive components. In an embodiment, the
frequency synthesizer may include elements such as a crystal
oscillator, a phase-locked loop (PLL), a frequency doubler, and/or
a combination thereof. In an embodiment, the frequency synthesizer
is digitally controlled by digital frequency control signals
received from the digital baseband system. The analogue processing
component may include elements such as mixers and filters, e.g.,
low pass filters (LPFs). In an embodiment, components of the RF
front-end are implemented in hardware as electronic circuits that
are fabricated on the same semiconductor substrate.
[0057] The digital baseband system 650 includes an
analog-to-digital converter (ADC) 662, a digital signal processor
(DSP) 664, and a microcontroller unit (MCU) 666. Although the
digital baseband system is shown as including certain elements, the
digital baseband system may include some other configuration,
including some other combination of elements. The digital baseband
system is connected to the CPU 652 via a bus.
[0058] FIG. 7 depicts an expanded view of an embodiment of portions
of the sensor system 610 of FIG. 6, including elements of the RF
front-end 648 that are configured to operate in the 2-6 GHz
frequency range. In the embodiment of FIG. 7, the elements include
a crystal oscillator 770, a phase locked loop (PLL) 772 (e.g., a
digitally controlled PLL), a bandpass filter (BPF) 774, power
amplifiers (PAs) 778, TX antennas 744, a frequency divider 784, a
mixer 786, an RX antenna 746, a low noise amplifier (LNA) 788, a
mixer 792, and an Intermediate Frequency/Baseband (IF/BB) component
794. As illustrated in FIG. 7, the group of receive components
identified within dashed box 796 is repeated four times, e.g., once
for each of four distinct RX antennas.
[0059] Operation of the system shown in FIG. 7 is described with
reference to a transmit operation and with reference to a receive
operation. In an embodiment, stepped frequency scanning refers
collectively to the transmit and receive operations. The
description of a transmit operation generally corresponds to a
left-to-right progression in FIG. 7 and description of a receive
operation generally corresponds to a right-to-left progression in
FIG. 7. With regard to the transmit operation, the crystal
oscillator 770 generates an analog signal at a frequency of 10 MHz.
The 10 MHz signal is provided to the PLL 772 and to the frequency
divider 784. The PLL uses the 10 MHz signal to generate an analog
signal that is in the 2-6 GHz frequency range. In an embodiment,
the PLL is digitally controlled in response to digital frequency
control signals (e.g., N bit control signals, where N is an integer
of 1 or more) that set the desired output frequency of the PLL. The
2-6 GHz signal is provided to the BPF 774, which filters the input
signal and passes a signal in the 2-6 GHz range to the PAs 778. The
2-6 GHz signal is also provided to the mixer 786.
[0060] The power amplifiers 778 amplify the RF signals in the 2-6
GHz range that are output from the TX antennas 744. In some
embodiments, RF energy is transmitted from both antennas
simultaneously and in other embodiments, RF energy is transmitted
from only one TX antenna at a time, or from different subsets of TX
antennas depending on how many TX antennas there are in the system.
In an embodiment, the 2-6 GHz signals are output at 20 dBm
(decibels (dB) with reference to 1 milliwatt (mW)). In an
embodiment and as described below, the PLL 772 is digitally
controlled to generate discrete frequency pulses between 2-6 GHz
that are used for stepped frequency scanning. For example, as is
described in more detail below, the 2-6 GHz frequency range can be
divided into multiple distinct frequencies, e.g., up to 1,024
discrete frequencies that can be individually identified and
selected through digital frequency control signals.
[0061] Dropping down in FIG. 7, the 10 MHz signal from the crystal
oscillator 770 is also provided to the frequency divider 784, which
divides the frequency down, e.g., from 10 MHz to 2.5 MHz via, for
example, two divide by two operations, and provides an output
signal at 2.5 MHz to the mixer 786. The mixer 786 also receives the
2-6 GHz signal from the BPF 774 and provides a signal at 2-6
GHz+2.5 MHz to the mixer 792 for receive signal processing.
[0062] With reference to a receive operation, electromagnetic (EM)
energy is received at the RX antenna 746 and converted to
electrical signals, e.g., voltage and current. For example,
electromagnetic energy in the 2-6 GHz frequency band is converted
to an electrical signal that corresponds in frequency (e.g., GHz),
magnitude (e.g., power in dBm), and phase to the electromagnetic
energy that is received at the RX antenna. The electrical signal is
provided to the LNA 788. In an embodiment, the LNA amplifies
signals in the 2-6 GHz frequency range and outputs an amplified 2-6
GHz signal. The amplified 2-6 GHz signal is then mixed with the 2-6
GHz+2.5 MHz signal at mixer 792 to generate a 2.5 MHz signal that
corresponds to the electromagnetic energy that was received at the
RX antenna. For example, when a 2 GHz signal is being transmitted
from the TX antennas and received at the RX antenna, the mixer 792
receives a 2 GHz signal that corresponds to the electromagnetic
energy that was received at the antenna and a 2 GHz+2.5 MHz signal
from the mixer 786. The mixer 792 mixes the 2 GHz signal that
corresponds to the electromagnetic energy that was received at the
RX antenna with the 2 GHz+2.5 MHz signal from the mixer 786 to
generate a 2.5 MHz signal that corresponds to the electromagnetic
energy that was received at the RX antenna. The 2.5 MHz signal that
corresponds to the electromagnetic energy that was received at the
RX antenna is provided to the IF/BB component 794 for
analog-to-digital conversion. The above-described receive process
can be implemented in parallel on each of the four receive paths
796. As is described below, the system described with reference to
FIG. 7 can be used to generate various discrete frequencies that
can be used to implement, for example, stepped frequency radar
detection, including stepped frequency radar ranging and stepped
frequency radar imaging, e.g., 2D or 3D imaging. As described
above, multiple mixing operations are performed to implement a
sensor system as described herein. The multiple mixers and
corresponding mixing operations implement a "compound mixing"
architecture that enables use of such frequencies.
[0063] FIG. 8 depicts an embodiment of the IF/BB component 794
shown in FIG. 7. The IF/BB component 894 of FIG. 8 includes similar
signal paths 802 for each of the four receive paths/RX antennas and
each signal path includes a low pass filter (LPF) 804, an
analog-to-digital converter (ADC) 862, a mixer 806, and a
decimation filter 808. The operation of receive path 1, RX1, is
described, although the description applies to each receive
path.
[0064] As described above with reference to FIG. 7, the 2.5 MHz
signal from mixer 792 (FIG. 7) is provided to the IF/BB component
794/894, in particular, to the LPF 804 of the IF/BB component 894.
In an embodiment, the LPF filters the 2.5 MHz signal to remove
negative frequency spectrum and noise outside of the desired
bandwidth. After passing through the LPF, the 2.5 MHz signal is
provided to the ADC 862, which converts the 2.5 MHz signal (e.g.,
IF signal) to digital data at a sampling rate of 10 MHz (e.g., as
12-16 bits of "real" data). The mixer 806 multiplies the digital
data with a complex vector to generate a digital signal (e.g.,
12-16 bits of "complex" data), which is also sampled at 10 MHz.
Although the signal is sampled at 10 MHz, other sampling rates are
possible, e.g., 20 MHz. The digital data sampled at 10 MHz is
provided to the decimation filter 808, which is used to reduce the
amount of data by selectively discarding a portion of the sampled
data. For example, the decimation filter reduces the amount of data
by reducing the sampling rate and getting rid of a certain
percentage of the samples, such that fewer samples are retained.
The reduction in sample retention can be represented by a
decimation factor, M, and may be, for example, about 10 or 100
depending on the application, where M equals the input sample rate
divided by the output sample rate.
[0065] The output of the decimation filter 806 is digital data that
is representative of the electromagnetic energy (e.g., in
frequency, amplitude, and/or phase) that was received at the
corresponding RX antenna. In an embodiment, samples are output from
the IF/BB component 894 at rate of 1 MHz (using a decimation factor
of 10) or at a rate of 100 kHz (using a decimation factor of 100).
The digital data is provided to a DSP and/or CPU 864 via a bus 810
for further processing. For example, the digital data is processed
to perform ranging and/or imaging, which may involve isolating a
signal from a particular location, e.g., isolating signals that
correspond to electromagnetic energy that was reflected from a
particular object (e.g., a person or a weapon carried by a person).
In an embodiment, stepped frequency scanning across a frequency
range includes the processes of transmitting stepped frequency
pulses at discrete frequencies, receiving RF energy, and outputting
corresponding digital data. Stepped frequency scanning may also
include processing of the generated digital data to generate
ranging information, imaging information, and/or some intermediate
information. In an embodiment, signal processing techniques may be
applied to implement beamforming, Doppler effect processing, and/or
leakage mitigation to isolate a desired signal from other undesired
signals.
[0066] In conventional RF systems, the analog-to-digital conversion
process involves a high direct current (DC), such that the I
("real") and Q ("complex") components of the RF signal at DC are
lost at the ADC. Using the system as described above with reference
to FIGS. 6-8, the intermediate frequency, IF, is not baseband, so I
and Q can be obtained after analog-to-digital conversion and
digital mixing as shown in FIG. 8.
[0067] In an embodiment, certain components of the sensor system
are integrated onto a single semiconductor substrate and/or onto a
single packaged IC device (e.g., a packaged IC device that includes
multiple different semiconductor substrates (e.g., different die)
and antennas). For example, elements such as the components of the
RF front-end 648, and/or components of the digital baseband system
650 (FIGS. 6-8) are integrated onto the same semiconductor
substrate (e.g., the same die). In an embodiment, components of the
sensor system are integrated onto a single semiconductor substrate
that is approximately 5 mm.times.5 mm.
[0068] In an embodiment, digital signal processing of the received
signals may involve implementing Kalman filters to smooth out noisy
data. In another embodiment, digital signal processing of the
received signals may involve combining receive chains digitally.
Other digital signal processing may be used to implement
beamforming, Doppler effect processing, and ranging. Digital signal
processing may be implemented in a DSP and/or in a CPU.
[0069] As described above with reference to FIGS. 6 and 7, the
frequency synthesizer (FIG. 6, 658) of the RF front-end (FIG. 6,
648) can generate discrete frequencies for transmission as
frequency pulses (also referred to as discrete frequency pulses) in
response to digital frequency control signals received from the
digital baseband system (FIG. 6, 650). In an embodiment, the
addressable frequency range of the sensor system is divided into a
number of individually addressable discrete frequencies. For
example, the addressable frequency range of 2-6 GHz is divided into
64, 128, 256, 512, or 1,024 individually addressable discrete
frequencies. The number of individually addressable discrete
frequencies in turn determines the step size (or vice versa), such
that 64 discrete frequencies in the 2-6 GHz frequency range
corresponds to a step size of 62.5 MHz/step (4 GHz/64=62.5 MHz).
Thus, as used herein the term "range scale" or "RS" refers to the
number of individually/digitally addressable frequencies that can
be generated using digital frequency control signals. That is, the
range scale (RS) is the scale at which the digitally addressable
frequency range is divided. FIG. 9 illustrates the frequency range
of 2-6 GHz relative to range scales of RS64, RS128, RS256, RS512,
and RS1024. In the example illustrated in FIG. 9, for the frequency
range of 2-6 GHz, the example range scales and corresponding step
sizes are: [0070] RS64=64 total steps at 62.5 MHz/step; [0071]
RS128=128 total steps at 31.25 MHz/step; [0072] RS256=256 total
steps at 15.625 MHz/step; [0073] RS512=512 total steps at 7.8125
MHz/step; and [0074] RS1024=1,024 total steps at 3.90625
MHz/step.
[0075] Using the approach illustrated in FIG. 9, each discrete
frequency is individually and uniquely identifiable by a number
(e.g., which can be communicated as a digital signal in binary
form) depending on the range scale. For example, the frequencies of
2 GHz, 3 GHz, 4 GHz, 5 GHz, and 6 GHz can be individually
identified by the respective numeric values depending on the range
scale: [0076] 1/16/32/48/64 at RS64; [0077] 1/32/64/96/128 at
RS128; [0078] 1/64/128/192/256 at RS256; [0079] 1/128/256/384/512
at RS512; and [0080] 1/256/512/768/1024 at RS1024.
[0081] To further illustrate how numeric values can be used to
individually identify discrete frequencies for use in stepped
frequency radar, FIG. 10 depicts the frequency range of 2-6 GHz
relative to a range scale of 256 (RS256). As illustrated in FIG.
10, numeric value "1" corresponds to 2 GHz, numeric value "64"
corresponds to 3 GHz, numeric value "128" corresponds to 4 GHz,
numeric value "192" corresponds to 5 GHz, and numeric value "256"
corresponds to 6 GHz. Using the above-described approach to
identify discrete frequencies, step sizes can be generated as
multiples of the step size of the particular range scale (RS). For
example, at RS64, it is possible to digitally identify discrete
frequency steps at multiples of 62.5 MHz/step, whereas at RS256, it
is possible to digitally identify discrete frequency steps at
multiples of 15.625 MHz (e.g., 15.625 MHz/step, 31.25 MHz/step, or
62.5 MHz/step), at RS512, it is possible to digitally identify
discrete frequency steps at multiples of 7.8125 MHz (e.g., 7.8125
MHz, 15.625 MHz/step, 31.25 MHz/step, or 62.5 MHz/step), and at
RS1024, it is possible to digitally identify discrete frequency
steps at multiples of 3.90625 MHz (e.g., 3.90625 MHz, 7.8125 MHz,
15.625 MHz/step, 31.25 MHz/step, or 62.5 MHz/step). In an
embodiment, a single range scale (RS) is used to digitally identify
a wide range of discrete frequencies and a wide range of step
sizes. For example, the range scale 1,024 (RS1024) is used to
digitally identify a wide range of discrete frequencies and a wide
range of step sizes. Examples of using digital frequency control
signals to implement stepped frequency scanning in a stepped
frequency radar system are described below.
[0082] In accordance with an embodiment of the invention, the step
size and/or frequency range of stepped frequency scanning is
changed during a scanning operation. For example, the step size is
changed from a first step size to a second step size and/or the
frequency range that is scanned is changed from a first frequency
range to a second frequency range. FIG. 11 is a process flow
diagram of operation of stepped frequency radar scanning. At block
1102, stepped frequency scanning is performed across a frequency
range using frequency steps of a step size. At decision point 1104,
it is determined whether or not the step size and/or the frequency
range should be changed. Various criteria can be used to determine
if and when the step size and/or frequency range should be changed.
If at decision point 1104 it is determined that the step size
and/or frequency range should not be changed, then the process
returns to block 1102. If on the other hand, it is determined that
the step size and/or frequency range should be changed, then the
process proceeds to block 1106. At block 1106, stepped frequency
scanning is performed with the changed step size and/or frequency
range. In an embodiment, the frequency of the transmitted frequency
pulses and the step sizes are controlled by digital frequency
control signals and changes to the step size and/or frequency range
are made based on preprogrammed digital frequency control signals
and in other embodiments, changes to the step size and/or frequency
range are made in response to feedback information from the
received signals.
[0083] In an embodiment, at least one parameter of the stepped
frequency scanning is changed in response to feedback information
from the received signals of the stepped frequency scanning. For
example, the step size and/or scanned frequency range may be
changed in response to identifying an object or in response to an
indication that an object may be present. FIG. 12 depicts a
feedback loop between the transmit and receive elements of the
sensor system described above with reference to FIGS. 6-8. In
particular, the sensor system depicted in FIG. 12 is the same as
the sensor system depicted in FIG. 7 except that the sensor system
depicted in FIG. 12 includes the digital baseband system 650 and a
feedback loop that is formed by the digital output of the IF/BB
component 794 of the RF front-end, the digital baseband system 650,
and digital frequency control signals that are provided to the PLL
772 from the digital baseband system 650. Using the feedback loop
illustrated in FIG. 12, the discrete frequencies that are generated
by the PLL can be digitally controlled by the digital baseband
system in response to an evaluation of digital data received from
the IF/BB component 794 of the RF front-end. The particular logic
used to evaluate the received digital data and to change the step
size and/or frequency range can be dependent on many factors,
including the particular application in which the sensor system is
deployed. Some examples of logic associated with changing the step
size and/or frequency range are described below. Although FIG. 12
illustrates a feedback based control scheme, in other embodiments,
the step size and/or frequency range of the stepped frequency
scanning can be changed according to preprogrammed frequency
control signals and/or pre-established rules.
[0084] As described above, digital control of discrete frequencies
in stepped frequency radar scanning enables flexible scanning that
can be adapted to implement various features and/or to achieve
various goals. At frequencies in the 2-6 GHz range, larger step
sizes may be more effective for ranging (i.e., determining the
range of an object) and smaller step sizes may be more effective
for imaging (i.e., determining the dimensions of an object,
particularly in 2D, e.g., relative to a plane that is perpendicular
to a line between the sensor system and the object). Thus, in one
application, it may be desirable to identify the range of an object
using frequency pulses transmitted at a first step size and to
identify a 2D or 3D profile of the object or a related object using
frequency pulses transmitted at a second, smaller, step size, and
possibly at a third, even smaller, step size. For example, in a
security sensor application, it may be desirable to use frequency
pulses transmitted over a wide frequency range at a first step size
to identify the range of an object (e.g., a person and/or a weapon)
and then use frequency pulses transmitted over a narrower frequency
range at a second, smaller, step size to identify the 2D or 3D
profile of an object (e.g., a person and/or a weapon carried by the
person). In an embodiment, the particular step sizes and/or
frequency ranges are selected/changed/adjusted in real time based
on feedback from the received signals (e.g., "on-the-fly"
adjustment). For example, the step sizes and/or frequency ranges
can be changed on-the-fly in a couple of repetition intervals, T.
The received signals may change as different frequencies reflect
off different objects in different ways (e.g., some frequencies
will resonate from a weapon better than other frequencies) and
therefore the parameters of the stepped frequency scanning can be
adapted on the fly to the current conditions that are being
experienced. In an embodiment, smaller step sizes around a specific
narrower frequency range may be better suited for 2D or 3D imaging
of an object such as a weapon due to the relatively high
reflectivity of portions of a weapon (e.g., around a particular
frequency range) that tend to be smooth, such as the barrel.
Alternatively, parameters (e.g., step size and frequency range
(frequency range could refer to the difference between two
frequencies or frequency range could refer to a specific frequency
range that is defined by two absolute frequencies)) of the stepped
frequency scanning can be pre-programmed.
[0085] FIGS. 13A and 13B illustrate two different examples of a
stepped frequency scanning operation, referred to as a
"telescopic," "zoom," or "focused" stepped frequency scanning
operation, which involves scanning a relatively wide frequency
range at a first step size and scanning a more narrow frequency
range (or frequency ranges) at a smaller step size or step sizes.
The example illustrated in FIG. 13A is referred to as an
"overlapping" stepped frequency scanning operation and the example
illustrated in FIG. 13B is referred to as a "non-overlapping"
stepped frequency operation.
[0086] With reference to FIG. 13A, a first scan (scan 1) of the
frequency range of 2-6 GHz is performed at a step size of 62.5 MHz
(.DELTA.f=62.5 MHz), a second scan (scan 2) of the frequency range
of 4-5 GHz is performed at a step size of 31.25 MHz (.DELTA.f=31.25
MHz), and then a third scan (scan 3) of the frequency range of
approximately 4.2-4.3 GHz is performed at a step size of 15.625 MHz
(.DELTA.f=15.625 MHz). As illustrated in FIG. 13A, scans 1, 2, and
3 each separately scan the frequency range of 4.2-4.3 GHz and thus
the three scans "overlap" in the 4.2-4.3 GHz frequency range.
[0087] With reference to FIG. 13B, a first scan (scan 1) of the
frequency range of 2-4 GHz is performed at a step size of 62.5 MHz
(.DELTA.f=62.5 MHz), a second scan (scan 2) of the frequency range
of 4-5 GHz is performed at a step size of 31.25 MHz (.DELTA.f=31.25
MHz), a third scan (scan 3) of the frequency range of approximately
4.2-4.3 GHz is performed at a step size of 15.625 MHz
(.DELTA.f=15.625 MHz), a fourth scan (scan 4) of the frequency
range of 4.3-5 GHz is performed at a step size of 31.25 MHz
(.DELTA.f=31.25 MHz), and then a fifth scan (scan 5) of the
frequency range of 5-6 GHz is performed at a step size of 62.5 MHz
(.DELTA.f=62.5 MHz). As illustrated in FIG. 13B, scans 1, 2, 3, 4,
and 5 all scan over different, non-overlapping, frequency ranges
and thus are "non-overlapping" over the range of 2-6 GHz.
[0088] In an embodiment, when using the sensor system for a
security application that involves identifying weapons such as
handguns, rifles, and knives, including weapons carried by a
person, the stepped frequency scanning may implement some form of
the above-described "telescopic," "zoom," or "focused" stepped
frequency scanning when the reflected signals indicate that a more
reflective object (e.g., a smooth object) is within range of the
sensor system. In one embodiment, an increase in the magnitude of
RF energy at certain wavelengths that correspond to known sizes of
weapons such as handguns, rifles, and knives (e.g., due to such
frequencies resonating off the weapon), may indicate that such an
object is within range of the sensor system. Therefore, in an
embodiment, the step size to be used in stepped frequency scanning
and the frequency range to be scanned are adjusted when certain
reflective characteristics are detected. In one embodiment, the
frequency range is reduced to a frequency range more closely
focused on a frequency range of interest (e.g., a frequency range
that is known through training to correspond to resonant
wavelengths of a weapon) and the step size is reduced to a step
size that can produce 2D profile information that can be used to
determine (e.g., to some degree of certainty) if a weapon may be
present. In an embodiment, in a security sensor application, it may
be desirable to use frequency pulses transmitted at a first step
size to identify the range of an object (e.g., a person and/or a
weapon) and upon receiving RF energy that indicates a person is
present or that an object that may be weapon is present, the sensor
system changes on the fly to transmitting frequency pulses at a
second, smaller, step size over a narrower frequency range (e.g.,
around frequencies that are known to resonate from a weapon such as
a handgun, rifle, or knife) to identify the 2D or 3D profile of an
object (e.g., a person and/or a weapon). In an embodiment, the
particular step sizes and/or frequency ranges are
selected/changed/adjusted in real time in response to information
received via the feedback loop of the sensor system as described
with reference to FIG. 12.
[0089] As described above with reference to FIGS. 9 and 10, the
individually addressable discrete frequencies used in the stepped
frequency scanning can be controlled by digital frequency control
signals. FIGS. 14A and 14B illustrate digital frequency control
signals that correspond to the stepped frequency scanning
operations illustrated in FIGS. 13A and 13B, respectively. In the
examples of FIGS. 14A and 14B, a range scale of 256, RS256, is used
as the range scale to identify the individually addressable
discrete frequencies that are transmitted from the sensor system.
With reference to FIG. 14A (which corresponds to FIG. 13A), the
discrete frequencies of scans 1, 2, and 3 are identified in a
sequential (in time) stream of numeric frequency identifiers. Using
an RS256 notation, discrete frequencies 4, 8, 12, . . . , 248, 252,
and 256 are generated and transmitted as frequency pulses to
implement scan 1 at a step size of .DELTA.f=62.5 MHz. Next,
discrete frequencies 128, 130, 132, . . . , 188, 190, and 192 are
generated and transmitted as frequency pulses to implement scan 2
at a step size of .DELTA.f=31.25 MHz. Lastly, discrete frequencies
136, 137, 138, 139, 140, 141,and 142 are generated and transmitted
as frequency pulses to implement scan 3 at a step size of
.DELTA.f=15.625 MHz.
[0090] With reference to FIG. 14B (which corresponds to FIG. 13B),
the discrete frequencies of scans 1, 2, 3, 4, and 5 are identified
in a sequential (in time) stream of numeric frequency identifiers.
Using an RS256 notation, discrete frequencies 4, 8, 12, . . . ,
124, and 128 are generated and transmitted as frequency pulses to
implement scan 1 at a step size of .DELTA.f=62.5 MHz. Next,
discrete frequencies 128, 130, 132, 134, and 136 are generated and
transmitted as frequency pulses to implement scan 2 at a step size
of .DELTA.f=31.25 MHz. Next, discrete frequencies 136, 137, 138,
139, 140, 141, and 142 are generated and transmitted as frequency
pulses to implement scan 3 at a step size of .DELTA.f=15.625 MHz.
Next, discrete frequencies 142, 144, 146, . . . , 188, 190, and 192
are generated and transmitted as frequency pulses to implement scan
4 at a step size of .DELTA.f=31.25 MHz. Lastly, discrete
frequencies 192, 196, 200, . . . , 248, 252, and 256 are generated
and transmitted as frequency pulses to implement scan 5 at a step
size of .DELTA.f=62.5 MHz. As illustrated in FIGS. 13A-14B, digital
control of discrete frequencies in a stepped frequency radar system
enables "telescopic," "zoom," or "focused" stepped frequency
scanning to transmit frequency pulses at a first step size to
identify the range of an object (e.g., a person and/or a weapon)
and then to change the step size and scanned frequency range on the
fly to a smaller step size over a narrower frequency range (e.g.,
around frequencies that are known to resonate from a weapon such as
a handgun, rifle, or knife) to identify the 2D or 3D profile of an
object (e.g., a person and/or a weapon).
[0091] As described above, digital control of discrete frequencies
in stepped frequency radar scanning enables flexible scanning that
can be adapted to implement various features and/or to achieve
various goals. In some cases, it may be desirable to skip or "hop"
a particular frequency band to, for example, avoid a frequency band
that may experience interfering RF energy. FIG. 15A illustrates an
example of "frequency hopping" in a stepped frequency scanning
operation relative to the 2-6 GHz frequency range and a range scale
of 256 (RS256). In the example of FIG. 15A, stepped frequency
scanning is performed over a frequency range of 2-6 GHz at step
size of 62.5 MHz, .DELTA.f=62.5 MHz, with the frequency band of 4-5
GHz being skipped or "hopped" over. In a stepped frequency scanning
operation, the frequency range of 2-4 GHz is scanned at 62.5 MHz
steps and then the frequency range of 5-6 GHz is scanned at 62.5
MHz steps. In an embodiment, the stepped frequency scanning is
performed at the same sweep rate throughout the scan. That is, the
time between frequency steps is constant (e.g., interval, T, see
FIGS. 2, 3B, 4A, and 3B) even through the frequency hop.
[0092] As described above with reference to FIGS. 9, 10, 14A, and
14B, the discrete frequencies used in the stepped frequency
scanning can be controlled by digital frequency control signals.
FIG. 15B illustrates digital frequency control signals that
correspond to the stepped frequency scanning operation illustrated
in FIG. 15A. In the example of FIG. 15B, a range scale of 256,
RS256, is used as the range scale to identify discrete frequencies
and the discrete frequencies of the scan are identified in a
sequential (in time) stream of numeric frequency identifiers. Using
an RS256 notation, discrete frequencies 4, 8, 12, . . . , 120, 124,
and 128 are generated and corresponding frequency pulses are
transmitted to implement the scan of the 2-4 GHz frequency range at
a step size of .DELTA.f=62.5 MHz and discrete frequencies 192, 196,
200, . . . , 248, 252, and 256 are generated and corresponding
frequency pulses are transmitted to implement the scan of the 5-6
GHz frequency range at a step size of .DELTA.f=62.5 MHz. In the
example of FIG. 15B, the digitally controlled frequency hop is
indicated by a dashed vertical line, which indicates where the
digital frequency control signals jump from numeric value 128 to
192 in one step. Although the numeric values of the digital
frequency control signals jump from numeric value 128 to 192, the
jump happens in one step (e.g., one fixed time interval, T) so that
there is no added time gap associated with the frequency hop.
[0093] The concept of frequency hopping in stepped frequency radar
operations is described above with reference to FIGS. 15A and 15B.
In environments that implement a wireless communications protocol
such as WIFI, the frequency bands of 2.412-2.462 GHz and
5.180-5.825 GHz may include RF energy that could interfere with the
sensor system described herein. Therefore, in an embodiment,
stepped frequency radar scanning can be performed in a manner that
"hops over" known interfering frequency bands, e.g., the
interfering frequency bands of 2.412-2.462 GHz and 5.180-5.825 GHz.
FIG. 16 illustrates an example of a case in which frequency hopping
is implemented in stepped frequency radar using digital frequency
control signals to avoid frequency bands of known interference.
Specifically, the example of FIG. 16 illustrates frequency hopping
over the WIFI frequency bands of 2.412-2.462 GHz and 5.180-5.825
GHz, although the techniques can be applied to other known
interfering frequency bands.
[0094] In the example described with reference to FIG. 16, the WIFI
frequency bands of 2.412-2.462 GHz and 5.180-5.825 GHz are known.
However, in other applications, the existence of interfering RF
energy in the surrounding environment may not be known. Thus, in an
embodiment, the existence of interfering RF energy in the
surrounding environment is learned by the sensor system and then
the sensor system can adapt the stepped frequency scanning to hop
over frequency bands that are identified to exhibit RF energy that
may interfere with stepped frequency radar operations. FIG. 17
illustrates a process in which a frequency range is first scanned
to identify an interfering frequency band and then the subsequent
scan (or scans) hops over the identified interfering frequency
band. In an embodiment and as illustrated in FIG. 17, first, a
learning scan (scan 1) is performed over the entire addressable
frequency range, e.g., 2-6 GHz. In an embodiment, the learning scan
is performed with the transmitter PAs deactivated (e.g., the PAs
678 in the sensor system depicted in FIG. 6 turned off or otherwise
bypassed) and the sensor system scanning the 2-6 GHz frequency
range for interfering signals. For example, with reference to FIG.
7, the PLL generates discrete frequency pulses in a stepped
frequency manner and the frequency pulses are distributed
throughout sensor system as described with reference to FIG. 7
except that amplified frequency pulses are not transmitted from the
TX antennas because the PAs are deactivated. In the example of FIG.
7, it is assumed that interfering RF energy is found in the
approximately 4.3-4.6 GHz frequency band and so the stepped
frequency scanning is digitally controlled to hop over the 4.3-4.6
GHz frequency band. In scan 2, the sensor system is digitally
controlled to hop over the interfering frequency band using the
techniques described above with reference to FIGS. 15A and 15B.
[0095] It has been found that larger frequency steps can be better
for ranging and smaller frequency steps can be better for 2D or 3D
imaging of certain objects of interest such as humans and weapons
such as handguns, rifles, and knives. However, performing separate
stepped frequency scans for ranging and imaging takes additional
time. Therefore, in an embodiment, stepped frequency scanning is
performed to simultaneously implement stepped frequency scanning
for two different purposes, e.g., for "ranging scanning" and for
"imaging scanning," which enables the generation of both ranging
data and imaging data. FIG. 18A illustrates stepped frequency
scanning over the 2-6 GHz frequency range in which ranging scanning
is performed over the entire 2-6 GHz frequency range simultaneously
with imaging scanning that is performed over only the 4-5 GHz
frequency range. In particular, in the example of FIG. 18A, ranging
scanning is performed at a first step size, e.g., .DELTA.f=62.5
MHz, and imaging scanning is performed at a second, smaller, step
size, e.g., .DELTA.f=15.625 MHz. In order to perform simultaneous
ranging scanning and imaging scanning, in an embodiment, over the
frequency range of 2-4 GHz, discrete frequencies are stepped at
62.5 MHz/step, then over the frequency range of 4-5 GHz, discrete
frequencies are stepped at 15.625 MHz/step, and then over the
frequency range of 5-6 GHz, discrete frequencies are stepped again
at 62.5 MHz/step. As illustrated in FIG. 18A, a single
non-overlapping scan across the frequency range of 2-6 GHz includes
frequency bands that are scanned at different step sizes.
[0096] FIG. 18B illustrates digital frequency coding (in a time
sequence) for the stepped frequency scanning illustrated in FIG.
18A. At the transmitter (TX), discrete frequencies are stepped at
62.5 MHz/step, then discrete frequencies are stepped at 15.625
MHz/step, then discrete frequencies are stepped at 62.5 MHz/step.
The digital frequency coding using an RS256 scale includes a first
scan segment of frequencies 4, 8, 12, . . . , 120, 134, and 128
(.DELTA.f=62.5 MHz), a second scan segment of frequencies 129, 130,
131, . . . , 190, 191, and 192 (.DELTA.f=15.625 MHz), and a third
scan segment of frequencies 196, 200, 204, . . . , 248, 252, and
256 (.DELTA.f=62.5 MHz). Reflections corresponding to the
transmitted frequency pulses are received in the same sequential
order at the receiver (RX) of the sensor system 1810 and processed.
With reference to the receive operation, FIG. 18B illustrates that
the discrete frequency pulses of the transmitted stream are
received in the same sequential order (in time) as they are
transmitted. The receiver, RX, then places ranging data in a
"ranging data bucket" 1820 and places imaging data in a different
"imaging data bucket" 1822. In particular, as illustrated in FIG.
18A, the ranging scan involves discrete frequency pulses at a step
size of 62.5 MHz across the frequency range of 2-6 GHz and the
imaging scan involves discrete frequency pulses at a step size of
15.625 MHz across the frequency range of 4-5 GHz. Thus, with
reference to the left side of the receive operation, the portion of
digital data that corresponds to the ranging data is placed in a
data ranging bucket that includes data corresponding to the
discrete frequencies of 4, 8, 12, . . . 248, 252, and 256 (based on
RS256) and the portion of digital data that corresponds to the
imaging data is placed in an imaging data bucket that includes data
corresponding to the discrete frequencies of 129, 130, 131, . . . ,
190, 191, and 192 (based on RS256). In this example, the discrete
frequencies of 132, 136, 140, . . . , 184, 188, and 192 will be
placed in both the ranging data bucket and the imaging data bucket
such that only the data associated with every fourth discrete
frequency from the scanned range of 129, 130, 131, . . . , 190,
191, and 192 (.DELTA.f=15.625 MHz) will be placed in the data
ranging bucket. In an embodiment, the demultiplexing or extracting
of the data into the proper buckets for further processing is
implemented in the digital baseband system or in a CPU and the
ranging and imaging buckets may be implemented as logical
constructs in the digital baseband system and/or the CPU. Thus, the
digital control of step size and frequency range in a stepped
frequency radar system enables simultaneous capture of ranging data
and imaging data via a non-overlapping stepped frequency scanning
operation using a single sensor system. Although the demultiplexing
or extracting of stepped frequency scanning data into specific
buckets is described with reference to simultaneous capture of
ranging and imaging data, the concept of demultiplexing or
extracting of stepped frequency scanning data into specific buckets
for subsequent processing can be implemented for other
applications.
[0097] In an embodiment, the entire frequency range, e.g., the
entire 2-6 GHz frequency range, could be scanned with a step size
of, for example, .DELTA.f=16.625 MHz (RS256), and ranging and
imaging data could be extracted at different multiples of the step
size from the set of digital data that is generated from the scan.
For example, for ranging, only data generated from every fourth
frequency pulse is processed, e.g., a step size of .DELTA.f=62.5
MHz, and for imaging, data generated from every frequency pulse in
the 4-5 GHz frequency range is processed, e.g., a step size of
.DELTA.f=16.625 MHz in the 4-5 GHz frequency range. In an
embodiment, the multiples used for extraction are integer
multiples, e.g., 1, 2, 3, 4, etc. of the step size at which the
frequency range was scanned. FIG. 18C illustrates digital frequency
coding (in a time sequence) for the stepped frequency scanning
illustrated in FIG. 18A in which a single stepped frequency scan is
performed across the 2-6 GHz frequency range at a step size of
.DELTA.f=16.625 MHz (RS256). At the transmitter (TX), discrete
frequencies are stepped at 16.625 MHz/step across the entire 2-6
GHz frequency range. Using the RS256 scale, the discrete frequency
pulses are identified as 1, 2, 3, 4, . . . 253, 254, 255, 256.
Reflections corresponding to the transmitted frequency pulses are
received in the same sequential order at the receiver (RX) of the
sensor system 1810 and processed. With reference to the receive
operation, FIG. 18C illustrates that the discrete frequency pulses
of the transmitted stream are received in the same sequential order
(in time) as they are transmitted. The receiver then places ranging
data in a "ranging data bucket" 1820 and places imaging data in a
different "imaging data bucket" 1822. In particular, as illustrated
in FIG. 18A, the ranging scan involves discrete frequency pulses at
a step size of 62.5 MHz across the frequency range of 2-6 GHz and
the imaging scan involves discrete frequency pulses at a step size
of 15.625 MHz across the frequency range of 4-5 GHz. Thus, with
reference to the left side of the receive operation, the portion of
digital data that corresponds to the ranging data is placed in the
data ranging bucket 1820 that includes data corresponding to the
discrete frequencies of 4, 8, 12, . . . 248, 252, and 256 (based on
RS256) (e.g., an extraction multiple of "4" over the frequency
range of interest) and the portion of digital data that corresponds
to the imaging data is placed in the imaging data bucket 1822 that
includes data corresponding to the discrete frequencies of 129,
130, 131, . . . , 190, 191, and 192 (based on RS256) (e.g., an
extraction multiple of "1" over the frequency range of interest).
In this example, the discrete frequencies of 132, 136, 140, . . . ,
184, 188, and 192 will be placed in both the ranging data bucket
and the imaging data bucket and only the data associated with every
fourth discrete frequency will be placed in the data ranging
bucket. The demultiplexing or extracting of the data into the
proper buckets for further processing is implemented in digital
baseband system or in a CPU and the ranging and imaging buckets may
be implemented as logical constructs in the digital baseband system
and/or the CPU. Thus, the digital control of step size and
frequency range in a stepped frequency radar system enables
simultaneous capture of ranging data and imaging data via a
non-overlapping stepped frequency scanning operation using a single
sensor system.
[0098] In an embodiment, multiple sensor systems such as the sensor
system described with reference to FIGS. 6-8 may be located near
enough to each other such that the transmitted stepped frequency
pulses may interfere with one another. For example, the sensor
systems may be located near enough to each other in a house or
building that transmitted frequency pulses and reflected RF energy
may intermingle between the two sensor systems. FIG. 19A depicts an
area 1902 (such as a room, a house, or a building) that includes
two sensor systems (including TX.sub.1/RX.sub.1 and
TX.sub.2/RX.sub.2), such as the sensor systems described above with
reference to FIGS. 6-8, which may interfere with each other during
stepped frequency scanning. Thus, if TX.sub.1 and TX.sub.2 transmit
frequency pulses at the same discrete frequency and at the same
time, the receivers, RX.sub.1 and RX.sub.2, may experience
interference, which may degrade the quality of the ranging and/or
imaging of the stepped frequency radar systems. However, in an
embodiment, digital control of the frequencies of the discrete
frequency pulses is used to encode the frequencies of the frequency
pulses, e.g., in a preprogrammed or pseudorandom fashion, so that
the frequency pulses of the two sensor systems are less likely or
unlikely to interfere with each other. That is, the frequency
pulses are not transmitted in-order or in-step, e.g., in sequential
order (i.e., one step size increment per frequency pulse
transmission), but rather are transmitted "out-of-order" or
"out-of-step," which can reduce the likelihood of two frequency
pulses from two different sensor systems interfering with each
other.
[0099] FIG. 19B illustrates encoding and corresponding decoding of
discrete frequency pulses transmitted from TX.sub.1 and TX.sub.2 of
the sensor systems 1910 depicted in FIG. 19A. In the example of
FIG. 19B, both TX.sub.1 and TX.sub.2 are simultaneously scanning
across the 2-6 GHz frequency range at a step size of 15.625
MHz/step (e.g., RS256). Thus, each transmitter will transmit 256
discrete frequency pulses to complete a scan across the entire 2-6
GHz frequency range, with the discrete frequency pulses being
identified by the numeric values of 1-256. As illustrated in FIG.
19B, TX.sub.1 transmits the 256 discrete frequency pulses in a
first pseudorandom order (e.g., 64, 17, 211, 12, 78, 94, . . . 2,
101, 112, 243, 16, 29, 84, 6, 251) and simultaneously with
TX.sub.1, TX.sub.2 transmits the same 256 discrete frequency pulses
in a second pseudorandom order (e.g., 14, 219, 18, 256, 212, 47, .
. . 5, 58, 141, 172, 3, 249, 11, 6, 4). In a case where the two
sensor systems 1910 are close enough to each other, interfering RF
energy (either reflected RF energy or RF energy directly from the
other transmitter) may be received at the sensor systems. For
example, with reference to RX.sub.1, RF energy corresponding to the
stream of discrete frequencies transmitted from TX.sub.1 and RF
energy corresponding to the stream of discrete frequencies
transmitted from TX.sub.2 may be received simultaneously at
RX.sub.1. However, because the receivers are using stepped
frequency radar, RX.sub.1 is simultaneously receiving on the same
frequency at which TX.sub.1 is transmitting such that when TX.sub.1
transmits at frequency 64, RX.sub.1 receives at frequency 64.
RX.sub.1 may also be simultaneously exposed to RF energy at
frequency 14 (generated from TX.sub.2), but the RF energy at
frequency 14 will not be received (e.g., will not interfere with
receiving RF energy at frequency 64) since frequency 14 does not
match the current transmission frequency (f.sub.TX1=64) of
TX.sub.1. The receiver, RX.sub.1, is then able to generate scan
data associated with each transmitted frequency pulse and re-order
the data in a sequential order (e.g., 1, 2, 3, . . . , 254, 255,
256) that allows ranging and/or imaging data to be gleaned from the
received RF energy. As illustrated in FIG. 19B, RX.sub.1 is able to
re-order the data in an order that corresponds to the frequencies
of the range scale, e.g., 1, 2, 3, . . . 254, 255, 256. Likewise,
when TX.sub.2 transmits at frequency 14, RX.sub.2 receives at
frequency 14. RX.sub.2 may also be simultaneously exposed to RF
energy at frequency 64 (generated from TX.sub.1), but the RF energy
at frequency 64 will not be received (e.g., will not interfere with
receiving RF energy at frequency 14) since frequency 64 does not
match the current transmission frequency (f.sub.TX2=14) of
TX.sub.2. The receiver, RX.sub.2, is then able to generate scan
data associated with each transmitted frequency pulse and re-order
the data in a sequential order (e.g., 1, 2, 3, . . . , 254, 255,
256) that allows ranging and/or imaging data to be gleaned from the
received RF energy. As illustrated in FIG. 19B, RX.sub.2 is able to
re-order the data in an order that corresponds to the frequencies
of the range scale, e.g., 1, 2, 3, . . . 254, 255, 256. Using the
above-described technique, encoding of the discrete frequency
pulses (e.g., preprogrammed or pseudorandom encoding) can be used
to avoid interference between two sensor systems that are located
within range of each other. In the example of FIG. 19B, given a
pseudorandom pattern of 256 discrete frequencies, the likelihood of
the two sensor systems transmitting frequency pulses at the same
frequency at the same time can be estimated as
1/256.times.1/256=1.5.times.10.sup.-7 chance of interference.
Although the example is described with only two sensor systems, the
encoding scheme can be applied to more than two sensor systems and
still provide a high degree of protection against interference
amongst sensor systems. In an embodiment, pseudorandom encoding may
implemented by pseudorandom number generators located within the
sensor systems.
[0100] In an embodiment, ranging refers to detecting the linear
distance between an object of interest and the sensor system using
stepped frequency scanning and imaging refers to detecting the
spatial spread of an object of interest relative to the sensor
system. In a three dimensional coordinate system of x, y, and z,
the ranging or range of an object relative to a sensor system may
be represented by digital information that corresponds to a linear
distance relative to the z axis and the imaging or image of an
object relative to the sensor system may be represented by digital
information that corresponds to the x and y dimensions of the
object. In an embodiment, 2D imaging may refer to information
corresponding to the x and y dimensions of an object without
ranging information and 3D imaging may refer to information that
combines ranging information with 2D imaging information to produce
three-dimensional information about an object relative to the
sensor system.
[0101] In an embodiment, an RF front-end is configured to support a
wider range of frequencies. FIG. 20 depicts and embodiment of an RF
front-end that is configured to support a 2-6 GHz frequency range
and a 122-126 GHz frequency range. The RF front-end is similar to
the FR front-end described with reference to FIG. 7 and thus
similar reference numbers are used to identify similar components.
In the embodiment of FIG. 20, the elements include a crystal
oscillator 770, a phase locked loop (PLL) 772, a bandpass filter
(BPF) 774, a mixer 776, power amplifiers (PAs) 778, TX antennas
744, a frequency synthesizer 780, a frequency doubler 782, a
frequency divider 784, a mixer 786, an RX antenna 746, a low noise
amplifier (LNA) 788, a mixer 790, a mixer 792, and an Intermediate
Frequency/Baseband (IF/BB) component 794. As illustrated in FIG.
20, the group of receive components identified within and dashed
box 796 is repeated four times, e.g., once for each of four
distinct RX antennas.
[0102] Operation of the system shown in FIG. 20 is described with
reference to a transmit operation and with reference to a receive
operation. The description of a transmit operation generally
corresponds to a left-to-right progression in FIG. 20 and
description of a receive operation generally corresponds to a
right-to-left progression in FIG. 20. With regard to the transmit
operation, the crystal oscillator 770 generates an analog signal at
a frequency of 10 MHz. The 10 MHz signal is provided to the PLL
772, to the frequency synthesizer 780, and to the frequency divider
784. The PLL uses the 10 MHz signal to generate an analog signal
that is in the 2-6 GHz frequency range. The 2-6 GHz signal is
provided to the BPF 774, which filters the input signal and passes
a signal in the 2-6 GHz range to the mixer 776. The 2-6 GHz signal
is also provided to the mixer 786.
[0103] Dropping down in FIG. 20, the 10 MHz signal is used by the
frequency synthesizer 780 to produce a 15 GHz signal. The 15 GHz
signal is used by the frequency doubler 782 to generate a signal at
120 GHz. In an embodiment, the frequency doubler includes a series
of three frequency doublers that each double the frequency, e.g.,
from 15 GHz to 30 GHz, and then from 30 GHz to 60 GHz, and then
from 60 GHz to 120 GHz. The 120 GHz signal and the 2-6 GHz signal
are provided to the mixer 776, which mixes the two signals to
generate a signal at 122-126 GHz depending on the frequency of the
2-6 GHz signal. The 122-126 GHz signal output from the mixer 776 is
provided to the power amplifiers 778, and RF signals in the 122-126
GHz range are output from the TX antennas 744. In an embodiment,
the 122-126 GHz signals are output at 15 dBm (decibels (dB) with
reference to 1 milliwatt (mW)). In an embodiment, the PLL is
controlled to generate discrete frequency pulses between 2-6 GHz
that are used for stepped frequency transmission.
[0104] The 10 MHz signal from the crystal oscillator 770 is also
provided to the frequency divider 784, which divides the frequency
down, e.g., from 10 MHz to 2.5 MHz via, for example, two divide by
two operations, and provides an output signal at 2.5 MHz to the
mixer 786. The mixer 786 also receives the 2-6 GHz signal from the
BPF 774 and provides a signal at 2-6 GHz+2.5 MHz to the mixer 792
for receive signal processing.
[0105] With reference to a receive operation, electromagnetic (EM)
energy is received at the RX antenna 746 and converted to
electrical signals, e.g., voltage and current. For example,
electromagnetic energy in the 122-126 GHz frequency band is
converted to an electrical signal that corresponds in frequency
(e.g., GHz), magnitude (e.g., power in dBm), and phase to the
electromagnetic energy that is received at the RX antenna. The
electrical signal is provided to the LNA 788. In an embodiment, the
LNA amplifies signals in the 122-126 GHz frequency range and
outputs an amplified 122-126 GHz signal. The amplified 122-126 GHz
signal is provided to the mixer 790, which mixes the 120 GHz signal
from the frequency doubler 782 with the received 122-126 GHz signal
to generate a 2-6 GHz signal that corresponds to the
electromagnetic energy that was received at the RX antenna. The 2-6
GHz signal is then mixed with the 2-6 GHz+2.5 MHz signal at mixer
792 to generate a 2.5 MHz signal that corresponds to the
electromagnetic energy that was received at the RX antenna. For
example, when a 122 GHz signal is being transmitted from the TX
antennas and received at the RX antenna, the mixer 792 receives a 2
GHz signal that corresponds to the electromagnetic energy that was
received at the antenna and a 2 GHz+2.5 MHz signal from the mixer
786. The mixer 792 mixes the 2 GHz signal that corresponds to the
electromagnetic energy that was received at the RX antenna with the
2 GHz +2.5 MHz signal from the mixer 786 to generate a 2.5 MHz
signal that corresponds to the electromagnetic energy that was
received at the RX antenna. The 2.5 MHz signal that corresponds to
the electromagnetic energy that was received at the RX antenna is
provided to the IF/BB component 794 for analog-to-digital
conversion. The above-described receive process can be implemented
in parallel on each of the four receive paths 796. As is described
here, the system described with reference to FIG. 20 can be used to
generate various discrete frequencies that can be used to
implement, for example, stepped frequency radar detection. As
described herein, multiple mixing operations are performed to
implement a sensor system at such a high frequency, e.g., in the
122-126 GHz range. The multiple mixers and corresponding mixing
operations implement a "compound mixing" architecture that enables
use of such high frequencies.
[0106] In an embodiment, the sensor system, or components thereof,
can be combined with other sensor systems to form a sensor system
that includes a larger sensor array. For example, multiple sensor
systems, such as the sensor systems as described above, can be
arranged into a 2D array to form a multi-sensor sensor system. In
one embodiment, four sensor systems are configured in a rectangular
2D array, such that the combined array includes eight TX antennas
and sixteen RX antennas. FIG. 23A depicts an embodiment of a
2.times.2 array of sensor systems 2110 (also referred to as RF
units, or RFUs) such as the sensors systems described above along
with a frequency controller 2104 that combine to form a
multi-sensor sensor system. In an embodiment, the frequency
controller can individually control the scanning frequencies of
each of the RF units. For example, the RF units can be controlled
to simultaneously transmit frequency pulses at different
frequencies to implement stepped frequency scanning in a manner
that avoids interference amongst the RF units. The frequency
controller can be implemented in hardware, software, firmware, or a
combination thereof.
[0107] As described above, the frequency controller 2104 can
control the RF units 2110 to simultaneously transmit frequency
pulses at different frequencies to implement stepped frequency
scanning in a manner that avoids interference amongst the RF units.
FIG. 21B illustrates an example operating scenario (in a graph of
frequency vs. time) in which the RF units simultaneously implement
stepped frequency scanning across different frequency sub-bands of
the 2-6 GHz frequency band in a manner that avoids interference. As
illustrated in FIG. 23B, RF unit 1 transmits stepped frequency
pulses in the frequency range of 2-3 GHz, RF unit 2 transmits
stepped frequency pulses in the frequency range of 3-4 GHz, RF unit
3 transmits stepped frequency pulses in the frequency range of 4-5
GHz, and RF unit 4 transmits stepped frequency pulses in the
frequency range of 5-6.
[0108] In the operating scenario illustrated in FIG. 21B, all of
the RF units scan across their corresponding frequency ranges using
a first step size, e.g., .DELTA.f=15.625 MHz/step (e.g., RS256) for
a period of time that corresponds to two full sweeps of the
corresponding frequency ranges. The same step size amongst the four
RF units is represented in that the scan lines all have the same
slope. Then, within the frequency ranges covered by RF units 2 and
3, there is something of interest detected from the received
signals. For example, the scanning may have detected a person
and/or a person carrying on object of interest such as a weapon.
Thus, as illustrated in FIG. 21B, the RF units 2 and 3 change their
step sizes to smaller step sizes and to narrow frequency ranges at
targeted frequency bands, which smaller step sizes and targeted
frequency bands may be better for identifying objects such as
weapons. As illustrated in FIG. 21B, the smaller step sizes for RF
units 2 and 3 are represented by the lower slope of the scan lines
that correspond to the stepped frequency scanning during the period
of time that corresponds to the next four sweeps and the smaller
frequency ranges and targeted frequency bands are represented by
the vertical displacement (frequency range) and vertical location
(targeted frequency bands) of the scan lines. Additionally, the
step sizes implemented by the RF units may change as indicated by
the change in slope between the third sweep and the fourth sweep.
At some point, the sensor system may decide to return to a sweep
configuration that is better suited for ranging as opposed to
imaging. FIG. 21B illustrates that in sweep seven, all of the RF
units in the system return to sweeping across their original
frequency bands at the original step size, e.g., .DELTA.f=15.625
MHz/step (e.g., RS256), which may be better suited for ranging as
opposed to imaging. As illustrated in FIG. 21B, the four RF units
perform simultaneous stepped frequency scanning across
non-interfering frequency ranges in a manner that enables multiple
frequency bands to be simultaneously scanned without interfering
with each other. Thus, digital control of discrete frequencies in a
stepped frequency radar system provides spectral agility that can
be utilized to implement a multi-sensor system that can be used to
implement ranging and 2D or 3D scanning in useful applications such
as security monitoring.
[0109] In an embodiment, signal processing to implement ranging and
2D or 3D imaging can be implemented in part or in full digitally by
a DSP and/or a CPU. FIG. 22 is an embodiment of a DSP 2264 that
includes a ranging component 2274 and an imaging component 2276.
Although the DSP is shown as including the two components, the DSP
may include fewer components and the DSP may include other digital
signal processing capability. The DSP may include hardware,
software, and/or firmware or a combination thereof that is
configured to implement the digital signal processing that is
described herein. In an embodiment, the DSP may be embodied as an
ARM processor (Advanced RISC (reduced instruction set computing)
Machine). In some embodiments, components of a DSP can be
implemented in the same IC device as the RF front-end and the TX
and RX antennas. In other embodiments, components of the DSP are
implemented in a separate IC device or IC devices.
[0110] In an embodiment, the transmission of millimeter radio waves
and the processing of signals that correspond to received radio
waves is a dynamic process that operates to locate signals
corresponding to the desired object (e.g., a person and/or a person
carrying a weapon) and to improve the quality of the desired
signals (e.g., to improve the SNR). For example, the process is
dynamic in the sense that the process is an iterative and ongoing
process as the location of the sensor system relative to a vein or
veins changes.
[0111] Beamforming is a signal processing technique used in sensor
arrays for directional signal transmission and/or reception.
Beamforming can be implemented by combining elements in a phased
antenna array in such a way that signals at particular angles
experience constructive interference while other signals experience
destructive interference. Beamforming can be used in both transmit
operations and receive operations in order to achieve spatial
selectivity, e.g., to isolate some received signals from other
received signals.
[0112] In an embodiment, the techniques described herein are
application to monitoring a health parameter of a person, for
example, monitoring the blood glucose level in a person, or to
monitoring other parameters of a person's health such as, for
example, blood pressure and heart rate. For example, the
reflectively of blood in a vessel such as the basilic vein will
change relative to a change in blood pressure. The change in
reflectivity as monitored by the sensor system can be correlated to
a change in blood pressure and ultimately to an absolute value of a
person's blood pressure. Additionally, monitored changes in blood
pressure can be correlated to heart beats and converted over time
to a heart rate, e.g., in beats per minute. In other embodiments,
the disclosed techniques can be used to monitor other parameters of
a person's health that are affected by the chemistry of the blood.
For example, the disclosed techniques may be able to detect changes
in blood chemistry that correspond to the presence of foreign
chemicals such as alcohol, narcotics, cannabis, etc. The
above-described techniques may also be able to monitor other
parameters related to a person, such as biometric parameters.
[0113] The above-described techniques may be used to monitor a
health parameter (or parameters) related to blood in a blood vessel
or in blood vessels of a person. The blood vessels may include, for
example, arteries, veins, and/or capillaries. The health monitoring
technique can target blood vessels such as the basilic and/or
cephalic veins and/or vessels other than the basilic and/or
cephalic veins. For example, other near-surface blood vessels
(e.g., blood vessels in the subcutaneous layer) such as arteries
may be targeted. Additionally, locations around the wrist or
locations other than the wrist area can be targeted for health
monitoring. For example, locations in around the ear may be a
desirable location for health monitoring, including, for example,
the superficial temporal vein and/or artery and/or the anterior
auricular vein or artery. In an embodiment, the sensor system may
be integrated into a device such as a wearable device (e.g., a
watch) or another device such as a smartphone or a standalone
health monitoring device.
[0114] In an embodiment, health monitoring using the techniques
described above, may involve a calibration process. For example, a
calibration process may be used for a particular person and a
particular monitoring device to enable desired monitoring
quality.
[0115] Although the techniques are described as using frequency
ranges of 2-6 GHz and 122-126 GHz, some or all of the
above-described techniques may be applicable to frequency ranges
other than 2-6 GHz and 122-126 GHz. For example, the techniques may
be applicable to frequency ranges around 60 GHz.
[0116] In an embodiment, a system similar to that described with
reference to FIG. 6 may be used to implement health monitoring by
transmitting and receiving RF energy in the 2-6 GHz range and/or in
the 122-126 GHz. For example, health monitoring may be implemented
using both the 2-6 GHz frequency range and the 122-126 GHz
frequency range. For example, in an embodiment, stepped frequency
scanning in implemented in the lower frequency range and then in
the higher frequency range, or vice versa. Using multiple
non-contiguous frequency ranges (e.g., both the 2-6 GHz frequency
range and the 122-126 GHz frequency range) may provide improved
accuracy of health monitoring.
[0117] Although the operations of the method(s) herein are shown
and described in a particular order, the order of the operations of
each method may be altered so that certain operations may be
performed in an inverse order or so that certain operations may be
performed, at least in part, concurrently with other operations. In
another embodiment, instructions or sub-operations of distinct
operations may be implemented in an intermittent and/or alternating
manner.
[0118] It should also be noted that at least some of the operations
for the methods described herein may be implemented using software
instructions stored on a computer useable storage medium for
execution by a computer. As an example, an embodiment of a computer
program product includes a computer useable storage medium to store
a computer readable program.
[0119] The computer-useable or computer-readable storage medium can
be an electronic, magnetic, optical, electromagnetic, infrared, or
semiconductor system (or apparatus or device). Examples of
non-transitory computer-useable and computer-readable storage media
include a semiconductor or solid state memory, magnetic tape, a
removable computer diskette, a random access memory (RAM), a
read-only memory (ROM), a rigid magnetic disk, and an optical disk.
Current examples of optical disks include a compact disk with read
only memory (CD-ROM), a compact disk with read/write (CD-R/W), and
a digital video disk (DVD).
[0120] Alternatively, embodiments of the invention may be
implemented entirely in hardware or in an implementation containing
both hardware and software elements. In embodiments which use
software, the software may include but is not limited to firmware,
resident software, microcode, etc.
[0121] Although specific embodiments of the invention have been
described and illustrated, the invention is not to be limited to
the specific forms or arrangements of parts so described and
illustrated. The scope of the invention is to be defined by the
claims appended hereto and their equivalents.
* * * * *