Emergency vehicle detector

Information

  • Patent Grant
  • 5559508
  • Patent Number
    5,559,508
  • Date Filed
    Wednesday, August 10, 1994
    30 years ago
  • Date Issued
    Tuesday, September 24, 1996
    28 years ago
Abstract
An emergency vehicle contains a transmitter for generating and transmitting a pair of fixed continuous wave signals which are distinguishable from each other in a preselected frequency band. A passenger vehicle contains a receiver which detects and distinguishes the pair of signals and generates an alert if the signals are determined to be at predetermined frequencies.
Description

FIELD OF THE INVENTION
The present invention relates generally to radar detectors, and more particularly, to a method and apparatus for detecting emergency vehicles with a radar detector.
BACKGROUND
It has long been desirable to provide a system whereby drivers are alerted to the presence of emergency vehicles, such as those used by police and fire personnel, so that safe operation of passenger vehicles can be maintained.
U.S. Pat. No. 4,238,778 discloses an emergency vehicle warning system which includes an RF transmitter in the emergency vehicle and a receiver in other vehicles. The transmitter includes a single oscillator for generating a carder frequency of predetermined frequency. The receiver includes an antenna and bandpass filter, and the intensity of signals passed by the filter are compared to a predetermined intensity level to validate the signal and generate a warning.
U.S. Pat. No. 5,235,329 discloses an emergency vehicle detection system wherein a passenger vehicle includes a receiver sensitive to the frequency of a wave-borne signal generated by the emergency vehicle. The emergency vehicle transmits a signal in a broad frequency band, and the receiver located in the passenger vehicle generates an alert for any signals received within that frequency band. However, each emergency vehicle is configured to have a unique dead band somewhere in selected frequency band, and each emergency vehicle has a received designed to generate an alert only for signals it receives in that dead band. In that way, an emergency vehicle will be alerted to other emergency vehicles but will not alert based on its own signal.
Radar detectors, such as the ESCORT.RTM. and PASSPORT.RTM. radar detector products manufactured and sold by Cincinnati Microwave, Inc., assignee herein, are generally known and used by vehicle drivers for detecting the presence of police radar signals and generating an alert thereto, as disclosed in the following commonly assigned patents: U.S. Pat. No. 4,313,216; U.S. Pat. No. 4,581,769; U.S. Pat. No. 4,954,828; U.S. Pat. No. 5,049,885; U.S. Pat. No. 5,079,553; and U.S. Pat. No. 5,305,007. However, legislation has banned the use of such devices in many states and in interstate trucking. It has been proposed that such devices be used for other purposes, such as to detect emergency vehicles. However, no one has successfully developed such an application. Therefore, it would be desirable to utilize a radar detector to detect emergency vehicles and generate an alert for such detection.
SUMMARY OF THE INVENTION
According to the present invention, a system is provided for detecting emergency vehicles. A transmitter is mounted in an emergency vehicle for generating and transmitting a first signal and a second signal, wherein the first signal and the second signal are fixed at different frequencies of a preselected frequency band. In the preferred embodiment, the K band is selected. A receiver is carried in a second vehicle for detecting that the first signal and the second signal are in a predetermined location and for generating an alert upon such detection. The second signal may be selectable between two discrete frequencies such that two combinations of first and second signals are provided. In one position, the detected signals indicate a moving emergency vehicle. In the other position, the detected signals indicate a stationary emergency vehicle. Alternatively, two types of transmitters could be provided, one type to generate the first and second signal which indicate a moving emergency vehicle, and the other type to generate a second and a third signal which indicate a stationary emergency vehicle.
A better understanding of the features and advantages of the present invention will be obtained by reference to the following detailed description of the invention and accompanying drawings which set forth an illustrative embodiment in which the principles of the invention are utilized.





BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a schematic diagram showing an emergency vehicle and a passenger vehicle equipped with the emergency vehicle detection system of the present invention.
FIG. 2 is a block diagram of a radar detector configured according to the present invention.
FIG. 3 A is a graphical representation of the transmitted signals from an emergency vehicle.
FIG. 3B is a graphical representation of the output from the quadrature detector portion of the present invention.
FIG. 4 is a simplified flow chart showing the steps performed in evaluating detected signal pairs.





DETAILED DESCRIPTION OF THE INVENTION
Referring now to FIG. 1, an emergency vehicle 2 is equipped with a transmitter 4 having two signal sources 6A and 6B for concurrently generating and transmitting a first signal S.sub.1 and a second signal S.sub.2, respectively. Preferably, the signals S.sub.1 and S.sub.2 are continuous wave signals fixed at specified frequencies located near opposite ends of the K band, which is defined by the Federal Communications Commission as 24.15+/-0.100 GHz. At a minimum, the signals S.sub.1 and S.sub.2 must be fixed at different frequencies in a preselected frequency band and be capable of discrimination by a receiver/detector unit.
In the preferred embodiment of the invention, two different types of signal sources are provided: one for moving vehicles and the other for stationary hazards. The receiver is adapted to detect and distinguish the different types of sources and to provide an alert corresponding to each type.
For example, in moving vehicles, transmitter source 6A generates the first signal S.sub.1 as a continuous wave signal fixed at 24.110+/-0.020 GHz and transmitter source 6B generates the second signal S.sub.2 as a continuous wave signal fixed at 24.230+/-0.020 GHz. For stationary vehicles, transmitter source 6A generates the first signal S.sub.1 as a continuous wave signal fixed at 24.070+/-0.020 GHz and transmitter source 6B generates the second signal S.sub.2 as a continuous wave signal fixed at 24.230+/-0.020 GHz. Thus, in the preferred embodiment, moving vehicles will transmit the first signal type, wherein the signals differ in frequency by 120 MHz, while stationary vehicles will transmit the second signal type, wherein the signals differ in frequency by 160 MHz. Other variations will be obvious to one skilled in the art, including the addition of more types of signal sources to differentiate other types of emergency vehicles or other mobile or stationary hazards. Further, the difference in frequency between signals need only be so large as to be distinguishable by the receiver. Filter technology is well known which can reduce the distinguishable difference to the order of a few MHz or less, but utilization of such technology is generally considered based on desired resolution and cost. For example, where the receiver generates both an s-curve and its image in response to a signal, as described below, a plurality of signals S.sub.1 . . . S.sub.n could be provided wherein the difference between signals is 40 MHz, and the receiver could adequately distinguish and alert for each signal or groups of signals. Image rejection schemes are also known, such as that employed in Cincinnati Microwave'S SOLO.RTM. radar detector, wherein the distinguishable difference is on the order of 20 MHz or less.
An emergency vehicle is preferably equipped with both types of signal sources and a means for selecting one or the other type. For example, a two position switch (not shown) may be operated between a first position if the emergency vehicle is moving and a second position if the emergency vehicle is stationary. Alternatively, a motion sensor (not shown) or other suitable switching means could be incorporated to automatically select between the two types of signal sources. In this way, passenger vehicles properly equipped as described below can determine from the received signals whether the emergency vehicle is moving or stationary.
A passenger vehicle 8 is equipped with a radar detector 10. As shown in FIG. 2, the radar detector 10 includes a microwave receiver section 12 coupled to a microprocessor section 14. The microprocessor section 14 includes sufficient hardware and/or software to evaluate the detected signals and generate an audible or visible alert on alert indicator 15. Typically, the microprocessor 14 may be programmed with appropriate instructions to evaluate signals which are detected by the receiver section 12.
Preferably, an application specific integrated circuit (ASIC) 17 is used to perform low rate signal processing, and a digital signal processor (DSP) chip 19 is used to perform high rate signal processing. Such a configuration is known, for example, from U.S. Pat. No. 5,305,007, the text of which is expressly incorporated herein by reference. Other detection configurations are generally known, for example, those shown in the following U.S. Patents which are also expressly incorporated herein by reference: U.S. Pat. No. 4,954,828; U.S. Pat. No. 5,049,885; and U.S. Pat. No. 5,079,553.
Generally, the receiver section 12 includes an antenna 16 for receiving incoming signals. A first local oscillator 18 is driven by a sweep circuit 20 to provide a signal which sweeps across the frequency band and which is mixed by first mixer 22 with the incoming signal to generate a first intermediate frequency signal IF.sub.1. Signal IF.sub.1 is amplified by IF amplifier 24 and mixed by second mixer 26 with a fixed signal from a second local oscillator 28 to generate a second intermediate frequency IF.sub.2. Signal IF.sub.2 is then amplified by amplifier 30, passed through bandpass filter 32, then amplified, limited and demodulated by quadrature detector 34 to generate as an output a pair of s-curves for each detected signal. As explained in U.S. Pat. No. 5,049,885, the s-curves define positions in time relative to the start of the sweep which correspond to the frequency at which the incoming signal is received.
As explained in U.S. Pat. No. 5,305,007, digital signal processing may be used to effectively evaluate the s-curves to determine whether they represent "valid" detected signals. Because the preferred embodiment of the present invention uses K band sources, the time spacing between s-curve pairs will be approximately 3.4 ms. However, rather than detecting just a single pair of s-curves in the K band, as would be the case for a conventional radar detector, the present invention will discriminate for two or more pairs of s-curves, as shown in FIGS. 3A and 3B. One transmitted signal S.sub.1 will be located at one end of the frequency band, and the other transmitted signal S.sub.2 will be located at the other end of the frequency band. Likewise, the output of the quadrature detector 34 will be the s-curve pair S.sub.3 and S.sub.3, corresponding to signal S.sub.1, and the s-curve pair S.sub.4 and S.sub.4, corresponding to signal S.sub.2, separated in a time domain as shown. This can be accomplished by making simple software changes in microprocessor 14 to realize the flow chart illustrated in FIG. 4. It should be obvious that many variations in the flow chart could provide an adequate solution. For example, an illustrative copy of source code is appended hereto and has been shown to work when implemented in Texas Instruments model TMS320C15 DSP chip. Referring to FIG. 4, the microprocessor 14 receives and stores two signals in step 100. An optional step 102 (but implemented in conventional radar detectors) checks to see if the signal(s) received are within the K band. If not, the program loops back. If so, then the microprocessor evaluates the s-curve pairs in step 104 to see if one of the pairs corresponds to 24.230+/-0.020 GHz. If not, the program may perform another process in step 105 (such as conventional police radar detection) and loop back. If so, then the microprocessor evaluates the other s-curve pair in step 106 to see if it corresponds to 24.110+/-0.020 GHz. If so, then an alert corresponding to a first signal type is generated in step 107. If not, then the microprocessor checks in step 108 to see if it corresponds to 24.070+/-0.020 GHz. If so, then an alert corresponding to a second signal type is generated in step 109. If not, then the program loops back.
It should be realized that many solutions could be realized via either hardware or software to implement the present invention. However, as most broadly contemplated, the present invention allows existing radar detectors to be modified through simple software changes to recognize these new emergency classes of signals. Other solutions will be obvious to those skilled in the art.
It should be understood that the invention is not intended to be limited by the specifics of the above-described embodiment, but rather defined by the accompanying claims.
__________________________________________________________________________Program Constants calculated in following section__________________________________________________________________________219 ; X & K band alerts can only occur in the middle third of the x/k/ka-inner220 ; sweep. Find the indicies of the boundaries of this region,221222 0020 0364 xkleft .word xcpts.sub.-- swp /3 ; Left edge223 0021 06c8 xkrite .word xcpts.sub.-- swp *2/3 ; Right edge224225 ; Beacon processing assumes that K band spacing of beacon type 1 is 120 mHz226 ; and beacon type 2 is 160 mHz. Calculate the width of each beacon type227 ; in terms of # of indicies. +++sko162a228229 0364 xkpoints .set xcpts.sub.-- swp*2/3 - xcpts.sub.-- swp/3; # x or k indicies in sweep230 00f6 kspectrum .set ksize/3 ; k-band is 1/3 of total sweep231 0022 01a7 beacon.sub.-- narrow .word 120*xkpoints/kspectrum ; # indicies separating beacon 1232 0023 0234 beacon.sub.-- wide .word 160*xkpoints/kspectrum ; # indicies separating beacon 2233 0024 0046 beacon.sub.-- toler .word 20*xkpoints/kspectrum ; #points in tolerance234__________________________________________________________________________Ram Variables & Flags__________________________________________________________________________586 0067 bit kb1,set5 ; Set if first K Source detected +++sko162a587 ; for Beacon Detection.588 0067 bit kbw,set5 ; Set if Wide Beacon Source detected +++sko162a589 0067 bit kbn,set5 ; Set if Narrow Beacon Source detected +++sko162a712 007d .bss beholdn,1 ; Beacon hold counter for narrow case713 007e .bss beholdw,1 ; Beacon hold counter for wide case0077 firstk equ tempz ; Index of first k band pair if beacon ; +++sko162a__________________________________________________________________________Machine Code for determining presence of 2 Beacon Source__________________________________________________________________________TypesG 456 06d9 6880 haples: larp ar0G 457 06da 3865- lar ar0,rindexG 458 ;G 459 ; Do Beacon detection processing. If 2 K band sources are detected with spaceG 460 ; `beacon.sub.-- wide` or `beacon.sub.-- narrow`, set associated flags kbw or kbn +++sko162aG 461 06db jpclr beacon,beadone ; If beacon disabled, prevent beacon processingG 462 06e0 jclr ksweep,beadone ; Is this K band processing?G 463 06e4 jclr kbl,kafrst ; If first K source flag kb1 set, testG 464 ; to see if beacon spacing requirements met.G 465 06e8 2088 lac *,0 ; Get the indexG 466 06e9 7901- and c1fffhG 467 06ea 1077- sub firstk ; Calculate spacing back to first k band sourceG 468 06eb 7f88 ahsG 469 06ec 5068- sacl tempiG 470 06ed ld beacon.sub.-- wideG 471 06f0 1068- sub tempiG 472 06f1 7f88 absG 473 06f2 5069- sacl tempj ; Store signal spacing in `tempi`G 474 06f3 ld beacon.sub.-- tolerG 475 06f6 1069- sub tempjG 476 06f7 fa00 blz notwid ; If within tolerance of `beacon.sub.-- wide`,06f8 06dd'G 477 ; Set `K Beacon Wide` FlagG 478 06f9 copyi 60,beholdwG 479 06fb f900 b beadone06fc 06f3'G 480 06fd notwid: ld beacon.sub.-- narrowG 481 0700 1068- sub tempiG 482 0701 7f88 absG 483 0702 5069- sacl tempjG 484 0703 ld beacon.sub.-- tolerG 485 0706 1069- sub tempjG 486 0707 fa00 blz beadone ; If within tolerance of `beacon.sub.-- narrow`,0708 06f3'G 487 ; Set `K Beacon Narrow` FlagG 488 0709 copyi 60,beholdn ; Set beacon hold to 40G 489 070b f900 b beadone070c 06f3'G 490 070d 2088 kafrst: lac *G 491 070e 7901- and clfffhG 492 070f 5077- sacl firstk ; Record index of left k band pairG 493 0710 set kblG 494 0713 beadone:__________________________________________________________________________Machine Code constructed to support Various Display Types__________________________________________________________________________H 462 ; Handle Beacon ProcessingH 463H 464 0a57 207e- wn: lac beholdw ; Decrement the wide & narrowH 465 0a58 ff00 bz atzero ; beacon detectors0a59 0a3c'H 466 0a5a 1005- sub one ; unlessH 467 0a5b 507e- sac1 beholdw ; they are allreadyH 468 0a5c 207d- atzero: lac beholdn ; equal to zero.H 469 0a5d ff00 bz atzerol0a5e 0a41'H 470 0a5f 1005- sub oneH 471 0a60 507d- sacl beholdnH 472 0a61 atzerol:H 473 0a61 207e- lac beholdw ; If both beacon hold counters +++sko170H 474 0a62 7a7d- or beholdn ; (either narrow or wide)H 475 0a63 ff00 bz bazero ; are at 0, clear the beacon indicators0a64 0a5f'H 476 0a65 207e- squir: lac beholdwH 477 0a66 107d- sub beholdn ; Alert type will be based on largest value.H 478 0a67 fc00 bgz calwid0a68 0a51'H 479 0a69 set kbnH 480 0a6c clr kbwH 481 0a6f f900 b wasnar0a70 0a57'H 482 0a71 calwid: set kbwH 483 0a74 clr kbnH 484 0a77 wasnar: clr xalert,kalert,kaalrt ; If in beacon `hold` interval, leaveH 485 0a7a set kalert ; in k-bank alert only. AllowH 486 0a7d f900 b qbe0a7e 0a6b'H 487 0a7f 7e60 bezero: lack kbn+kbw ; Was either kbn or kbw set in previous sweep?H 488 0a80 7923- and kbn.sub.-- iH 489 0a81 ff00 bz qbe0a82 0a6b'H 490 0a83 copy clfffh.xktime ; If so, Terminate alert here byH 491 0a85 5056- sacl tmout ; advancing xktime and tmoutH 492 0a86 clr kbn,kbwH 493 0a89 f900 b endalr0a8a 0b62'H 494 0a8b qbe:H 601 0aec jclr kbw,smear1 ; If beacon, substitute 2 appropriate sounds.H 602 0af0 copyi beacl,xsoundH 603 .if lcdH 604 0af2 copyi emer3,tempu ; Display `Road Hazzard` on LCD displayH 605 0af4 7e49' lack emer4H 606 0af5 f900 b ysim0af6 0ae0'H 607 .endifH 608 0af7 smearl: jclr kbn,smear2H 609 0afb copyi beac2,xsoundH 610 .if ledH 611 0afd copyi emerl,temptu ; Display `Emergency Vehicle` on LCD displayH 612 0aff 7e3c' lack emer2H 613 0b00 f800 ysim: call botl0b01 0e53'H 614 .endif__________________________________________________________________________
Claims
  • 1. In a radar detector having means for detecting the presence of a radio frequency signal within a preselected frequency band and means for generating an alert thereto, wherein in the improvement, the detecting means includes means for distinguishing at least two discrete radio frequency signals each of which is fixed at a different frequency within the preselected frequency band and means for generating a modified alert upon detecting and distinguishing the discrete signals, wherein the discrete signals are fixed so as to differ in frequency by at least 40 MHz.
  • 2. A system for emergency vehicle detection, comprising:
  • transmitter means mounted in an emergency vehicle for generating and transmitting a pair of radio frequency signals each fixed in a preselected frequency band and separated by a distinguishable amount, wherein the transmitter means includes means for selecting from a plurality of pairs of radio frequency signals, each pair being uniquely separated by a distinguishable amount;
  • receiver means carried in a second vehicle for detecting the pair of signals and for distinguishing the one signal from the other signal; and
  • means for generating an alert upon detecting and distinguishing the pair of signals.
  • 3. A system as in claim 2, wherein the pair of signals are fixed so as to differ in frequency by at least 40 MHz.
  • 4. A system as in claim 2, wherein the transmitter means includes means for selecting the frequency for one or more of the signals, and wherein a first signal is fixed at a first preselected frequency and a second signal is selectable between a second preselected frequency and a third preselected frequency.
  • 5. A system as in claim 4, wherein the first signal is fixed at 24.230+/-0.020 GHz and the second signal is selectable between 24.110+/-0.020 GHz and 24.070+/-0.020 GHz.
  • 6. A system as in claim 2, wherein a first pair of signals differs in frequency by 120 MHZ and a second pair of signals differs in frequency by 160 MHz.
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Entry
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