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BACKGROUND OF THE INVENTION
1. Field of the Invention
This invention is in the field of radio direction finding systems and
methods therefor, and more particularly is an improved radio direction
finding system utilizing Doppler frequency shift principles whereby
frequency modulation is imparted to the received signal by electronically
moving the effective receiving antenna location along a circular path such
that the modulation phase angle indicates the bearing of the radio
transmission.
2. Description of the Related Art
Radio direction finders (RDFs) are used to indicate the angle of arrival of
an incoming radio frequency wave front for the purpose of locating the
source of the transmission. A single RDF may be used on a mobile platform
to home in on the source of the transmission, or a network of RDFs may be
used to locate the transmission source by triangulation.
An excellent type of RDF is that utilizing the synthetic Doppler method. In
this system, a circular array of fixed antenna elements is switched
sequentially or combined electronically so as to simulate the rotation of
a single antenna element in a circle. See for example, U.S. Pat. No.
4,551,727 "Radio Direction Finding System" by David C. Cunningham. As the
simulated antenna approaches the direction of the incoming wave front, the
apparent frequency increases due to the well known Doppler Effect.
Similarly, when the simulated antenna moves in the same direction as the
wave front, its apparent frequency decreases. This up-down frequency
modulation is recovered by connecting the RDF antenna to a standard
frequency modulation receiver and can be heard as a tone at the audio
output of the receiver. The frequency of the tone is the same as the
rotational rate of the antenna, and the phase of the tone is related to
the direction of arrival. The RDF provides the signal processing to
measure this phase and display the hearing to the transmission source.
One of the many applications in which RDFs are utilized is to locate
vehicles (police cars, delivery vans or stolen cars). In the case of
stolen vehicle location, the transmitter is generally activated by the
police using radio control after the vehicle is reported missing. See for
example U.S. Pat. No. 4,818,998 by Apsell and Stapelfeld. Additional
applications include the tracking of shipped packages by freight carriers
or others where it is desired to verify the location of the shipped
package.
In such applications, it is necessary to distinguish which of many vehicles
is transmitting the signal that is being tracked. This is most commonly
accomplished by utilizing a pulsed transmission which is frequency
modulated by a digitally coded sequence to indicate the identity of the
vehicle. A variety of frequency shift keying techniques (FSK, MSK, GMSK,
CPFSK, etc.) are used to carry the digitally encoded identification number
of the transmitter on the pulsed signal. Sec for example, the MX-COM
Products and Applications book which discusses these techniques and
presents integrated circuits that are used to encode and decode FSK
signals (Available annually directly from MX-COM Inc. of Winston-Salem
N.C.)
There are several compatibility problems that arise when a synthetic
Doppler RDF is used with an FSK coded pulse transmission. The frequency
modulation of the encoded signal interferes with the recovery of the phase
information in the RDF due to the overlapping of the FSK modulation with
the frequency modulation of the simulated antenna rotation. Furthermore,
the frequency modulation due to the antenna rotation interferes with the
recovery of the FSK coded signal information. These problems can be
alleviated to some extent by judicious selection of the frequency
modulation frequencies (FSK tones) and the rotational speed of the RDF
antenna. However, this approach is limited by the audio bandpass of the
receiver, the modulation sidebands of both the FSK modulation and the RDF
antenna modulation, and non-linearities in the receiver.
Another problem is that the signal level required to provide acceptable FSK
demodulation is typically several dB higher than that needed to produce a
stable bearing display. This can result in the RDF displaying bearings
toward transmitters other than the one desired. Such extraneous signals
can be due to other transmission sources, intermodulation or harmonics of
broadcast signals, and interference.
Therefore, a need existed to provide a radio direction finder utilizing the
Doppler principle that is not subject to the bearing errors caused by the
FSK modulation. Additionally, a need existed to provide FSK decoding of
the transmitted identification data in a Doppler direction finder that is
not subject to the errors caused by the simulated rotation of the antenna.
SUMMARY OF THE INVENTION
An object of the present invention is to provide a radio direction finder
utilizing the Doppler principle that is not subject to the bearing errors
caused by the FSK modulation.
Another object of the present invention is to provide FSK decoding of the
transmitted identification data in a Doppler direction finder that is not
subject to the errors caused by the simulated rotation of the antenna.
BRIEF DESCRIPTION OF THE PREFERRED EMBODIMENTS
In accordance with one embodiment of the present invention, an improved
radio direction finder is disclosed. The improved radio direction finder
is comprised of an antenna means for receiving a locator transmission
signal having alternating periods of a broadcast RF carrier wave and a
broadcast modulated RF carrier wave, a radio direction finder (RDF) means
coupled to the antenna means for determining the direction to a
broadcasting transmitter and for extracting coded information from the
locator transmission signal wherein the RDF means comprises antenna
virtual rotation control means coupled to the antenna means for
controlling the antenna in both a non-rotational mode for detection of the
broadcast modulated RF carrier wave and a virtual rotation mode for
detection of the broadcast RF carrier wave. Additionally, the antenna
means comprises a plurality of antenna elements of at least 3. The RDF
means further comprises receiving circuitry means coupled to the antenna
means for receiving the locator transmission signal, and decoding
circuitry means coupled to the antenna means for decoding the coded
information. The RDF means further comprises microprocessor means coupled
to the antenna means for calculating a bearing angle to the broadcasting
means and antenna virtual rotation control means for selecting from among
the non-rotational mode for detection of the broadcast modulated RF
carrier wave and the virtual rotation mode for detection of the broadcast
RF carrier wave. The system further comprises summing means coupled to the
plurality of antenna elements for continuous switching of the antenna
elements and for mixing of the locator transmission signal received by the
antenna elements.
In accordance with another embodiment of the present invention, a method
for receiving and decoding a locator transmission signal is disclosed. The
method comprises the steps of providing an antenna for receiving the
locator transmission signal wherein the locator transmission signal
comprises a period of a broadcast RF carrier wave and a period of a
broadcast modulated RF carrier wave, holding the antenna stationary for
enhanced extraction of embedded information from the broadcast modulated
RF carrier wave, and virtually rotating the antenna during the period of
the broadcast RF carrier wave for determining the bearing angle to the
source of the broadcast RF carrier wave. The step of providing an antenna
further comprises the step of providing an antenna having at least 3
antenna elements. The method further comprises the steps of summing a
signal from each of the at least three antenna elements during the period
of non-rotation of the antenna to provide a summed signal from which to
extract the embedded information, and continuously switching and mixing a
signal from each of the at least 3 antenna elements to virtually rotate
the antenna wherein the virtual rotation of the antenna is used for
determining the bearing angle to the source of the broadcast RF carrier
wave.
The foregoing and other objects, features, and advantages of the invention
will be apparent from the following, more particular, description of the
preferred embodiments of the invention, as illustrated in the accompanying
drawings.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a simplified block diagram of the radio direction
finding/identification transmitter & receiver systems.
FIG. 2 shows the timing intervals and identifies the associated modes of
operation of the radio direction finding/identification decoding system.
FIG. 3 is a simplified block diagram of the counter implementation of the
audio phase detector, and the timing sequence of its use.
FIG. 4 is a simplified block diagram of the synchronous demodulator
implementation of the audio phase detector and shows a timing sequence of
its use.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
An improved system and method for receiving and decoding an FSK encoded
locator transmission signal is described below. The system is directed
towards a radio direction finder utilizing the Doppler principle that is
not subject to the bearing measurement errors caused by FSK modulation nor
the FSK decoding errors caused by the rotation, simulated or actual, of
the antenna. The improvement is achieved by using a system that makes use
of the fact that a locator transmission signal comprises a period of a
broadcast RF carrier wave, and a period of a broadcast modulated RF
carrier wave. The present invention is directed towards holding the
antenna stationary for enhanced extraction of embedded information from
the broadcast modulated RF carrier wave, and then virtually rotating the
antenna during the period of the broadcast RF carrier wave for determining
the bearing angle to the source of the broadcast RF carrier wave.
Referring to FIG. 1, the radio direction finding system is shown
(hereinafter the "system 10"). The system 10, consists of a multiple
element antenna 1 (hereinafter the "antenna 1"), a direction finding
electronics 20, and an FM receiver 50. The direction finding electronics
20 comprise an RF summing circuit 24, a waveform generator 25, an audio
phase detector 26, an angle display 27, an FSK decoder 28, an
identification code display 29 and a microprocessor 23. The FM receiver 50
is a separate self contained unit utilized with the present invention.
A broadcast transmitter outputting an appropriate locator transmission
signal, while not part of the present invention, is described herein to
aid in understanding the construction and operation of the present
invention. A typical broadcast transmitter 40 consists of a broadcast
antenna 48, an FM transmitter 42, an FSK encoder 44, and a timer 46. The
broadcast transmitter 40 outputs a locator transmission signal as shown in
FIG. 2 line 60. The broadcast transmitter 40 comprises an antenna 48
coupled to an FM transmitter 42. The FM transmitter 42 is coupled to the
FSK encoder 44 which supplies an identification code or other desired
information. Coupled to both the FM transmitter 42 and the FSK encoder 44
is the timer 46. The timer 46 controls the on and off operation of the FM
transmitter 42, and also controls the timing of the FSK encoder 44's
output of the identification code. The identification code controls the
modulation of the carrier wave broadcast by the FM transmitter 42.
The system 10 receives the broadcast locator transmission signal via the
multiple element antenna 1 which consists of the antenna elements 1a, b,
c, d. The antenna elements 1a, b, c, d are arranged in a pattern so as to
form a regular polygon. The minimum number of elements may actually be as
few as three elements in a triangular pattern, but 4 or 8 are typically
used depending on the accuracy requirements of the system. Each antenna
element 1a-d is designed to provide omnidirectional reception and the
spacing between adjacent antenna elements 1a-d is less than 1/2 a
wavelength. In a preferred embodiment, of the present invention the
spacing between adjacent antenna elements 1a-d is in the range of 1/8 to
3/8 wavelength.
Coupled to the antenna 1 is the RF summing circuit 24. The RF summing
circuit 24 combines the broadcast location transmission signals received
by each of the antenna elements 1a-d so as to generate a single broadcast
location transmission signal (see FIG. 2 line 62.) having a maximum
possible gain. This results in the maximum possible sensitivity of the
system 10 and results in the generated or combined single broadcast
location transmission signal approximating the gain of the signal which
would be induced into a larger single antenna element. This addition of
the signals from each antenna element 1a-d takes place when the antenna 1
is not rotating. The RF summing circuit 24 also contains the circuitry
(not shown) to control the gains from each individual antenna element
1a-d, and will cause the simulated antenna rotation when the gains are
varied in the correct sequence. The RF summing circuit 24 also sums the
signal outputs of the antenna elements 1a-d. A preferred method for
implementing the RF summing circuit 24 is to use (not shown herein) a
circuit possessing constant input impedance, variable gain preamplifiers
and a resistive or inductive summing network as described by the
inventor's previous U.S. Pat. No. 4,551,727. Alternative methods that may
be used for RF summing circuits and, which arc well known to those skilled
in the art, include the series PIN diodes described in Norris U.S. Pat.
No. 4,041,496 or the odd/even channel clement switches with two variable
gain circuits described in Bambara U.S. Pat. No. 4,292,639.
The RF summing circuit 24 is coupled to the waveform generator 25. The
waveform generator 25 provides the control voltages used to vary the gains
in the RF summing circuit 24. Typically, one waveform is used for each
antenna element 1a-d, and the waveforms are identical except they are
displaced in time. For example, in a preferred embodiment, a four antenna
element 1a-d system requires that each control waveform be phased 90
degrees apart. By simulating a rotating antenna using varying gains for
the antenna elements 1a-d the incoming location transmission signals are
frequency modulated due to the Doppler Effect. The modulation frequency is
equal to the rotational speed of the simulated antenna, the deviation is
proportional to the antenna spacing, and the phase of the modulation,
relative to the reference signal used to control the RF summing circuit
24, is equal to the bearing angle. The waveform generator 25 also supplies
timing reference 4 signals to the audio phase detector 26.
The RF summing circuit 24 is coupled to an FM receiver 50. The FM receiver
50 selects the specific signal frequency desired and demodulates the
frequency modulation induced by the simulated rotating antenna 1. The FM
receiver 50 in a preferred embodiment is an external, stand-alone, FM
receiver of the scanner or two-way transceiver variety, and must be
supplied by the user of the present invention. Alternatively, although not
shown herein, an FM receiver could be incorporated into the present
invention. The system 10 couples to the FM receiver 50 in a standard
manner as is well known to those skilled in the art. The RF summing
circuit 24 couples to the antenna input 2 of the FM receiver 50, and the
FM receiver 50 audio output 3 couples to the FSK decoder 28 and the audio
phase detector 26 via standard connections or jacks. The FM receiver 50,
previously coupled to the direction finding electronics 20, is used to
select the specific signal frequency desired and to demodulate the
frequency modulation induced by the simulated rotating antenna. If the
broadcast transmission locator signal also contains frequency modulation,
both the transmitted modulation and the antenna sweep frequency will be
present at the audio output 3 of the FM receiver 50.
Referring to FIG. 4, one embodiment of the audio phase detector 26 is
shown. This embodiment implements a synchronous demodulator for the audio
phase detector 26. The bandpass filter 80 is set to pass the audio
component at the antenna sweep frequency. Timing reference 4 is used as
the control input to the synchronous sine demodulator 81. The synchronous
sine demodulator 81 provides an output which is equal to its input when
its control input is logically true and equal to the inversion of its
input when its control input is logically false. The signal, which is
shown as the waveform 85, has an average value equal to the magnitude of
the audio output 3, times the sine of the angle between the audio output 3
and the timing reference 4. Low pass filter 87 removes the ripple
frequencies (at multiples of the sweep frequency) from the sine
demodulator output 85 and provides a DC signal to the A to D converter 89
which is equal to the desired average value. Similarly, the synchronous
cosine demodulator 82 has as its control input a phase shifted timing
reference 84. This phase shifting is accomplished by 90 degree phase
shifter 83. Since the synchronous cosine demodulator reference 84 is in
quadrature with the timing reference 4, the output of the synchronous
cosine demodulator 82 has an average value equal to the magnitude of the
audio output 3, times the cosine of the angle between the audio output 3
and the timing reference 4. Low pass filter 88 removes the high
frequencies from the cosine demodulator output 86 and provides a DC signal
to the A to D converter 90 which is equal to the desired average value.
The microprocessor 23 divides the sine signal by the cosine signal, and
takes the arctangent of this ratio. This results in the bearing angle
which it then converts into a form needed to drive the angle display 27.
Referring to FIG. 3, wherein like numerals and symbols as previously shown
in FIG. 4 have a prime ' mark added herein, an alternate embodiment of the
audio phase detector 26 is shown. This embodiment implements a counter
embodiment for the audio phase detector 26. The band pass filter 70 is set
to pass the audio component at the antenna sweep frequency. The one shot
71 is triggered by a positive going zero crossing of the filtered audio
signal. Timing reference 4' is a square wave at the antenna sweep
frequency and is used to set flip flop 73. Flip Flop 73 is reset by the
one shot output 72. The flip flop 73 output is used as one of the inputs
to AND gate 74. The second input to the AND gate 74 is a square wave
signal having a frequency equal to 360 times the sweep frequency provided
by oscillator 75. The gate output 76 of the AND gate 74 is therefor a
series of P pulses where P is equal to the bearing angle in degrees. The P
pulses are accumulated in counter 77 and its output is transferred into
latch 78 by the positive going transition of the inverted output of the
flip flop 73. The same inverted output of the flip flop 73 resets counter
77. The output of the latch is read by the microprocessor 23 which
converts the count P into the form needed to drive the angle display 27.
Referring to FIG. 1, the FSK decoder 28 is coupled to the audio output 3
from the FM receiver 50 and decodes the identification code modulated on
the broadcast transmission locator signal. The FSK decoder 28 is selected
to match the modulation format used by the broadcast transmission locator
signal. In a preferred embodiment, the signal modulation is 1200 baud
Minimum Shift Keyed (MSK) in which case the mark(1)/space(0) frequencies
are 1200 and 1800 Hz, respectively, and the FSK decoder 28 utilizes a
MX469 integrated circuit, made by MX-COM or an equivalent circuit as is
well known to those skilled in the art.
In an alternative embodiment, the signal modulation format is Bell 202 and
the data is sent at 1200 baud with mark(1)/space(0) frequencies of 1200
and 2200 Hz, respectively. In this alternative embodiment the FSK decoder
is the MX614 integrated circuit manufactured by MX-COM, Inc. of
Winston-Salem, N.C.
It should be noted, as is well known to those skilled in the art, that for
RF telemetry, MSK is preferred over the Bell 202 type of modulation.
The microprocessor 23 is coupled to the FSK decoder 28 and the audio phase
detector 26. The microprocessor 23 functions to convert or process the
demodulator data, and to convert the identification code data and bearing
angle information into the signal formats required by the identification
code display 29 and the angle display 27. The microprocessor 23 is also
coupled to the waveform generator 25 via the mode control 5 signal and the
direction control 6 signal both of which serve to control the rotation
mode and direction of the antenna 1.
The angle display 27 is coupled to the microprocessor 23 and provides the
bearing angle in a format convenient for readout. In a preferred
embodiment, as described herein, the angle display 27 consists of several
segmented or dot matrix LED or liquid crystal displays to present the
bearing in decimal form. An alternative embodiment (not shown) could
however use an array of light emitting diodes (LEDs) arranged in a circle
to simulate a compass rose.
The identification code display 29 provides the identification code in a
convenient format for viewing. Depending on the character set used for the
identification code, this display may consist of 4 to 8 decimal or
hexadecimal numbers or ASCII characters. In a preferred embodiment, as
described herein, the identification code display 29 consists of an LED
display such as the HCMS-29XX manufactured by Hewlett Packard Co.
The operational sequencing of the direction finding electronics 20 is as
shown in FIG. 2 lines 62 and 64. Under normal conditions, the direction
finding electronics 20 are in the FSK decode mode as shown in FIG. 2 line
64. In this mode, the waveform generator 25 provides signals to the RF
summing circuit 24 which correspond to one or more antenna elements 1a-d
on but with no simulated antenna 1 rotation (FIG. 2 line 62) Preferably,
all antenna elements 1a-d are commanded to the on condition which has been
found to result in a net gain of several dB over the gain when the antenna
elements 1a-d are simulating rotation. In this mode, the FSK decoder 28 is
presented with an audio signal input, from the audio output 3 of the FM
receiver 50, which is free of any modulation error due to the antenna 1
rotation. While in this mode, the system 10 will be looking for a locator
transmission signal (FIG. 2, line 62, TA), and once such a signal is
detected, the system 10 will detect and decode the desired identification
code or information (FIG. 2, line 62, TB.)
The direction finding electronics 20 remains in this mode of non-rotation
until a suitable signal has been decoded by the FSK demodulator (not
shown) of the FSK decoder 28. At this time, the waveform generator 25 is
caused to switch to its bearing measurement mode by the mode control 5
signal from the microprocessor 23, and the control waveforms to the RF
summing circuit 24 are such as to create the variable gains needed to
simulate rotation of the antenna 1 (FIG. 2, line 62, TC). Although the
invention is applicable to a hard switched system to simulate antenna
rotation, the RF summing circuit 24 preferably uses a continuous
electronic switching and mixing of the signal from the antenna elements
1a-d. The microprocessor 23 sends a direction control 6 signal to the
waveform generator 25 to select a simulated antenna 1 rotation in the
clockwise direction.
The unmodulated carrier wave input to the audio phase detector 26 is a
signal that contains only the frequency corresponding to the simulated
rotation of the antenna 1 and is free of FSK modulation and the errors
that would result from the presence of FSK modulation on the carrier wave.
Following a period of clockwise simulated rotation of the antenna 1, the
microprocessor 23 sends a direction control 6 signal to the waveform
generator 25 to select a simulated antenna 1 rotation in the
counter-clockwise direction. The waveform generator 25 remains in the
bearing measurement mode for a time period which is slightly shorter than
the nominal unmodulated carrier interval. It then returns to the FSK
decode mode (FIG. 2, line 62, TD).
The use of alternating clockwise (CW) counterclockwise (CCW) simulated
antenna 1 rotation, which is not normally possible with pulsed
transmissions, may be used in this system to reduce the bearing error
caused by receiver mistuning. An example of this type of antenna control
and bearing measurement is described by Cooney in U.S. Pat. No. 4,148,034.
If the continuous portion of the carrier wave broadcast is relatively long
(for example, 1 second), the waveform generator 25 may be controlled by
the microprocessor 23, via the direction control 6, to cause clockwise
rotation for 1/2 second followed by counterclockwise rotation for another
1/2 second. If however, the unmodulated time interval is short (for
example, 75 milliseconds), the waveform generator 25 may be controlled by
the microprocessor 23, via the direction control 6, to produce a clockwise
rotation for 75 milliseconds during the first received pulse and 75
milliseconds during the second received pulse. Following both clockwise
and counter-clockwise simulated rotation periods of the antenna 1, and if
the same identification code has been received for both simulated rotation
periods, the bearing measurements are averaged together to obtain a best
bearing number.
Switching between FSK decode and bearing measurement modes is based on a
decision that a suitable signal is being received. This decision may be
based on one or more of the following criteria:
Presence of an RF carrier exceeding a specified threshold.
Presence of audio energy within the FSK signaling bandwidth exceeding a
specified threshold.
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