May 23, 31950 7 B. CHANCE - j2,5®8,555 ELECTRICAL NAVIGATION SYSTEM Filed Sept. 21, 1945 _ 3 Sheets-Sheet 1 "CAT" FIG. I BEACON A ' , \ "MOUSE" > . IO MILES <~IO MILES - BEACON B‘ - " 19 ‘9* 4%? / RCLE VIDEO 8Q\ FROM GATE F|G.4' 8|\ _ GOINGIDENCE RANGE DELAY‘ GENERATOR ClRGUlT v 82\ DELAY ‘ 84\ DIFFERENTIAL H . 83\ CIRCUIT M530“ clRcun" —3wrrc|-\' *' GOINCIDENCE CIRCUIT INVENTOR. ’ BY BRITTON CHANCE ' 9x4”. ATTORNEY ay 23» 195 2,598,565 B. CHANCE ELECTRICAL NAVIGATION SYSTEM 3 Sheets-Sheet 2 Filed Sept. 21, 1945 \ mw?dm $8 \NN \E052 N @E __ o. , QS ._ I. n mm_ 3 _ _N mm! o[jJw| t 2 _ \ _ _ .m TMI_T I|LK _ /ml_m_wC|_zw §.m._, lIi|3lI||_ r u m~\Lu _F. J. _<zzm_:?< /= _ / _5N2m|E3am;a FI|l\i lk L $E252 hm8g86 V 2A@8t26i4.”m5;.e0 \m235/ow/%9‘0 42m“m58o4zmg1. \ / m\/mm _ _ m ?“ IN VEN TOR. BR’ITTON CHANGE ATTORNEY 23, 1950 B, CHANCE I ' 2,598,565 ELECTRICAL NAVIGATION SYSTEM Filed Sept. 21, 1945 3 Sheets-Sheet 3 VIDEO 9o\ FROM GATE RANGE DELAY ' 9| ,_,COINGIDENCE ' GENERATOR C'RQU'T 1 9% DIFFERENTIAL 92\ DELAY 93\ >~>COINOIDENCE ‘ cmcun ERROR cmcurr i/HZ ‘ /||4 COINCIDENCE CIRCUIT l k CONNECTOR ’ CIRCUIT ‘ | l l I l I n3 5 l// us com‘émamcz DELAY “3 CIRCUIT TO COkNEbTOR Mc'izggu'? - ’ CIRCUIT SWITCH” INVENTOR. BRITTON CHANCE BY ATTORNEY ‘Patented May 23, 1950 v 2.508.565 vuurrso sfrA'rEs Pars 2,508,565 ELECTRICAL NAVIGATION SYSTEM Britton Chance, Cambridge, Mass., assignor, by 'mesne assignments, to the United States of America-as represented by the Secretary of War Application September 21, 1945, Serial No. 617,873 10 Claims. (Cl. 343-45) 2 . This invention relates to an electrical naviga ods, radio responder beacons are designated as beacons A and B while 0 is, the point to which the aircraft P is to be accurately navigated. If bombs are to be dropped, point 0 becomes the bomb release point and is determined from the tion system and more particularly to a means for simultaneously tracking a plurality of respond ing radio beacons. One method of navigating an aircraft includes the determination of the distance between the aircraft and a radio beacon having a known posi tion. The beacon may be of the type which, when interrogated by a pulse of electromagnetic energy transmitted by the radio object detection apparatus carried by the aircraft, responds with a reply. position of the target, by predetermining the alti- I tude, speed, and heading of the ‘aircraft at the 1o The response of the beacon may be a series of pulses uniquely coded to distinguish it from other responding beacons. The time claps ing between the transmission of the interrogating pulse from the aircraft and the receipt by the air craft of the beacon response is a measure of the bomb release point, and by predicting the wind velocity and direction. One method by which the aircraft may accu= rately navigate to the bomb release point is by ?ying at a constant distance from one beacon, known as the cat beacon, and shown as A. in Fig.‘ l. The bombs are released when the aircraft ar ‘lives at the proper distance from beacon B, known as the mouse beacon. When the cat and mouse bombing approach is - distance from the aircraft to the beacon. used, voltages may be produced each of which is The aircraft may carry apparatus capable of proportional to the range from the aircraft to one being set to track a preselected beacon and pro 20 beacon. These voltages may each be compared ducing a continuous measure of the range of the with a fixed voltage preset to a value correspond beacon from the aircraft. As used herein the ing to the range of destination, or bomb release term “tracking a beacon” denotes the operation of point, to one of the beacons. producing a voltage the magnitude of which is - If a voltage corresponding to the entire range proportional to the instantaneous range fromthe 25 to a beacon, such as A-C in Fig. 1, is used for aircraft to the beacon. If the range from the air comparison with a ?xed‘ voltage, the percentage craft of two beacons having known positions is variation of the changing range voltage is small determined, the position of the aircraft may be and it is di?icult to make the comparison with a established. ‘ high degree of precision. It is therefore more It is an object of this invention to provide an‘ satisfactory if the range of the aircraft is tracked apparatus for simultaneously tracking a plurality with respect to a ?xed range circle such as range of beacons. It is a further object to provide circles l or 2 designated in Fig. l. Voltages cormeans for tracking a plurality of beacons where~ responding to the ranges of the aircraft to range by at least some of the tracking components are circles i and 2 are therefore compared with volt35 ages corresponding to the distances C-D and used in the tracking of each beacon. Other objects, features, and advantages'of this C-E. The percentage variation of the changinvention will suggest themselves to those skilled ing range voltages is then high and the compari in the art and will become apparent from the fol son with the ?xed voltages may be readily made lowing description of the invention taken in con with precision. I nection with the accompanying drawing in 40 Referring now more particularly’ to Fig. 2, ra which: _ /' dio object detection apparatus it includes timer Fig. l is a diagram used in explaining the prin H controlling the operation of transmitter 12 ciples of beacon navigation; which is connected through transmit-receive Fig. 2 is a block diagram of a navigation system (T-R) switch is to radiating element is of an 45 tenna l5. Timer ii is preferably a circuit capa involving the principles of this invention; Fig. 3 shows the viewing screen of the indicator ' tube in Fig. 2; _ Fig. 4 is a block diagram of one form 01’ beacon tracker circuit; ' Fig. 5 is a block diagram showing an alterna- ' tive form of a beacon tracker circuit; and Fig. 6 is a schematic wiring diagram of one . ’ ' ' ‘ : ' ble of producing short sharp voltage pulses at ac curately spaced intervals oi’ time. Antenna it also includes re?ecting element it and is rotated about a vertical axis by antenna drive mechanism ll. T—R switch it is also connected to receiver it. 'An indication of antenna rotation is trans mitted as indicated by dotted line 22 to di?'eren tial gear assemblies 23 and it, provided with ad form of memory circuit.‘ Referring now more particularly to Fig. 1 for justing knobs 25 and 28 respectively. The output an explanation of navigation and bombing meth- 55 ‘1 of di?erential 23 drives cam 29 while the output " 3 asoasss of differential 24 drives cam 30. Cams 2! and II both act upon cam follower ll pivoted at point 32 and held in a neutral position by member 33 and ‘the tension of spring 84. Follower 3i may be slightly ?exible so as not to break if, during ad justment, it is simultaneously forced in opposite directions by cams 29 and 30. Timer H is also connected to provide 9, refer ence pulse to step delay circuit 40 which may be vided with the output of receiver ll to provide an index pulse and may be any circuit capable of comparing the beacon response or index pulse from receiver l8 with the delayed reference pulse from range delay circuit 55 and producing 9. volt age proportional to the time di?erence in the oc currence of the two pulses. The output voltage of beacon tracker It must have one polarity if the reference pulse occurs before the beacon response any circuit capable of delaying the reference 10 and the opposite polarity if the reference pulse pulses from timer II by ‘predetermined steps. occurs after the beacon response. Beacon track One circuit that is well adapted for use as a step er circuit 50 will be more fully described below delay circuit is a uni-stable multivibrator circuit. with reference to Figs. 4 and 5. It is well known that this type of multivibrator Beacon tracker circuit 80, is provided with a will produce a voltage pulse starting at the time 15' switch 52 having upper position “A,” lower posi an input pulse is ap lied to a control element of tion "3,” and middle neutral position "N." In the multivibrator. t is also well known that the the upper position “A," switch 82 makes contact time width of the pulse produced by a uni-stable with memory circuit A. .Memory circuit A may multivibrator may be made proportional to the be any circuit capable of receiving the error VOlt‘. steady bias voltage applied to the same or another 20 age from beacon tracker circuit 80 and producing control element. This pulse generated by the a continuing voltage indicative of the elapsed time between the interrogating pulse and the re short, sharp output pulse occurs in time coinci ceived response, and hence indicative of the range dence with the trailing edge of the pulse gener from the aircraft to the beacon. The output ated by the multivibrator. If the bias voltage ap 25 voltage of memory circuit A also varies in mag plied to the multivibrator in discreet steps the in nitude in accordance with the rate of variation in ' terval of time between the time the input pulse range between the aircraft and beacon. In posi is applied and the time the sharp output pulse is tion “B,” switch 62 connects beacon tracker 8| generated will vary in discreet steps or discreet with memory circuit. B which is constructed in intervals of time. It will be convenient in analyz 30 the same manner as memory circuit A. Switch ing the operation of this circuit to speak of the 63 having upper position “A," lower position “B,” output pulse from the multivibrator as a delayed and middle neutral position “N" is provided to reference pulse. The delayed reference pulse is connect line 59 to the output of either memory fed to range delay circuit 58. Range delay circuit circuit A or memory circuit B. 85 58 may be a second uni-stable multivibrator circuit Memory circuits A and B which will presently similar to the one described , above._ However, be described in connection with Figure 6 may be range delay circuit 58 diil’ers from circuit 40 in constructed in the manner disclosed for the mem that the bias voltage applied to circuit 58 is‘con ory circuit in the application by Andrew B. Jacob tinuously variable rather than being variable in sen, Serial No. 584.233, entitled “Electrical cir steps as was the case in circuit 40. The continu 40 cuit," ?led March 22, 1945. ously variable bias voltage permits circuit 58 to Memory circuits A and B are more fully de produce a continuously variable time delay. Step scribed in connection with the, description of delay circuit 40 is provided with a switch 45 having Fig. 6 below. 1 . an upper position “A? lower position “3,” and The output of memory circuit A may be com middle neutral position “NJ’ Switch 45 in the “A” pared by meter 65 to a voltage picked up by ad position makes contact with the contactor 46 of ’ justable contactor 6B. Contactor 85 is adjustable potentiometer 41 connected between a source of along potentiometer 61 connected between a positive potential and ground. In the "3” posi source of positive potential and ground. The out tion, switch 45 makes contact with contactor 48 of put of memory circuit B is compared by meter 58 potentiometer 49 connected between a source of 50 with a voltage picked up by contactor 10. Con positive potential and ground. Contactors 46 and tactor ‘i0 is adjustable along potentiometer Tl 48 are adjustable along their respective potenti connected between a source of positive potential ometers in steps. Since the pulse repetition rate and ground. Bomb release circuit 72 receives an of timer i l is high compared to the switching rate input from memory circuit B and contactor ‘I0. 55 of switch 45 the delay introduced by circuit 40 Circuit ‘#2 may be any circuit capable of releasing when switch 65 is in the “A” position will be de a bomb, as by energizing or deenergizing a relay, termined by the bias supplied by potentiometer when the voltage output of memory circuit 13 is 5?. When switch 85 moves to the “B” position equal to the voltage picked up by contactor 10.‘ ' the delay introduced by circuit at will be that de Since relays and relay circuits that operate on a termined by potentiometer 49. ~ 60 very small differential between two applied volt Timer ii is also connected to sweep generator ages are very well known it is not considered nec 50, the output of which isconnected to the de essary to further describe circuit ‘I2. However, if: iiecting coils 5! of cathode ray indicator tube 52. it is desired to construct a bomb release circuit Tube 52 also contains electron gun 53, control that is well adapted for use with applicant's in 65 vention reference should be had to the copending grid 54, and ?uorescent screen 55. As stated above, range delay'circuit 58 may be application of Richard K. Mosher, Serial No. any circuit capable of adding a controlled delay $922,155, entitled, Electrical apparatus, ?led June to the pulse received from step delay circuit 40. Again, the pulse produced by circuit 58 could be In the operation of the apparatus set forth differentiated to produce a sharp pulse at the V10 in Fig. 2, timer I I controls the operation of trans trailing edge of the multivibrator pulse. mitter I: so that the latter produces a series of The delayed pulse provided in the output of equally spaced radiov frequency pulses which are range delay circuit 58 is applied to control grid 55 transmitted through T-R switch ii to antenna of indicator tube 52 and also to beacon tracker l5. Radiating element It and re?ector ll co circuit 60. Beacon tracker circuit 60 is also pro‘ 75 operate to Produce a narrow directional beam of multivibrator may be differentiated so that a radio frequency pulses. Antenna it is rota about a vertical axis by antenna drive l‘l. 1 radio responder beacons intercepting the search pulses sent out by antenna it will respond by transmitting a non-directional reply. Any reply received by antenna it will be fed through T-R switch as to receiver it. T-R switch it is pro-» vided for the purpose of preventing radio pulses produced by transmitter l2 from entering receiver age correctly 3) to the range of beacon A, the delay given the reference pulse will. be such as to cause the reference pulse to appear at bea con tracker to in time coincidence with the arrival of the index ‘pulse beacon response and no error voltage will be supplied to change the out put of fnemory circuit A. On the other hand, if the two pulses do not arrive coincidently at beacon tracker Bil, a proper error voltage will be it, and for preventing signals received by antenna l0 produced to correct the range voltage produced it from entering transmitter l2. by memory circuit A which will in turn correct Cams 29 and 3B are rotated in synchronism with the range delay in circuit 58. antenna it. The phase of cams 29 and 30 may be When beacon B is being interrogated, the ac adjusted by knobs 25 and 26 respectively so that tion is similar to that described above except when rotating antenna It approaches the azi 15 that switch t2 applies the error voltage produced muth oi’ beacon A, cam 29 coacts with cam fol by beacon tracker st to memory circuit B while switch 83 applies the range voltage from memory lower 85 to throw swit'ches d5, 82, and 63 into their "A” positions. The switches are kept in circuit B to range delay circuit 58 so that the range pulse has a delay corresponding to the their “A" position while antenna is sweeps through a short arc, the center of which has an range of beacon B. ' The range voltage produced‘ by memory cir cuit A is compared by meter 66 with the voltage set in potentiometer 61. Meter 85 will thus beacon B, cam 38 coacts with follower 3i and indicate when the aircraft reaches a certain range causes switches as, $2, and $3 to be in their “B” 25 with respect to beacon A. Meter til similarly azimuth approximately that of beacon A. The are may have a width of about 15°. Similarly when antenna it approaches the azimuth of position through a short are of rotation by an indicates when the aircraft reaches a certain tenna it. During the intervals when antenna in is not pointed approximately at either beacon A range with respect to beacon B. On bombing missions, bombrelease mechanism l2 automat ically releases the bombs when the aircraft reach or B, neither cam 2Q nor til will coast with fol lower 8i. and switches (it. 82, and to will be in 80 es the range preset into potentiometer l l. their neutral position “N.” The range of the beacon is tracked in the ap The reference pulse produced by timer ii isied paratus of Fig. 2 by delaying the reference pulse to step delay circuit dd where it is delayed by one from timer H by an amount corresponding to the predetermined amount when antenna id is point range from the aircraft to the beacon. Adjust ment of step delay circuit M by potentiometers ed at beacon A and by another controlled amount when antenna it is pointed at beacon B. The . delay for beacon A is set by adjustment of con tractor 58 while the delay for beacon B is set by adjustment of contractor lit. In the situation shown in Fig. l, contactor 58 would be set to , give a delay corresponding to AD while contactor 68 would be set to give a delay corresponding to BE. The delayed reference pulse in the output of circuit Ad is further delayed by range delay cir cuit 58. The additional delay given by circuit 58 depends upon the control voltage received through line 59, from either memory circuit A or memory circuit B in dependence upon whether antenna it. is pointed at beacon A or beacon, B. ‘The delayed reference pulse in the output of circuit 58 is fed to beacon tracker 86 where its time of arrival is compared with the time of arrival of the response received from the inter rogated beacon. If the delayed pulse from cir 6i and as introduces delays of an amount cor respondng to any of the 10 mile range circles shown in Fig. i. It will be obvious however that the step delay circuit is not necessarily limited to 10 mile steps but, may be made adjustable to in troduce delays corresponding to any range. In the situation shown in Fig. l, the step delay cir cuit tit introduces delays corresponding to the distances from beacons A and B to range circles l and 2 respectively. Range delay circuit 58 in troduces delays corresponding to the range from the aircraft P to range circles l and 2. Referring again to Fig. 1, when the cat and mouse method of approach to destination or the bomb release point is used, meter 65 indicating the range to beacon A becomes a pilot direction indicator, the de?ection of the needle indicating to the pilot whether or not he is on course, and in which direction he must go to get on course, while meter t6 becomes a distance-to-go meter cuit 58 arrives at beacon tracker til at the same indicating to the pilot the distance to the bomb time as the beacon response or index pulse from release point. receiver it, no error voltage is produced by beacon tracker so. If the delayed reference pulse arrives In Fig. 4 is shown a possible circuit for beacon tracker $3 in which ‘the reference pulse from before the beacon response, an error voltage of range delay circuit as produces in gate generator one polarity is produced, said voltage being of a magnitude proportional to the time difference. if the delayed reference pulse arrives at a time after the arrival of the beacon response, a voltage of the 8d a square pulse which is fed to coincidence circuit ti and delay circuit 92 where it is de ' iayed by a slight amount and fed to coincidence . opposite polarity is produced,'said voltage having circuit 83. Again, gate generator til may be a uni-stable multivibrator. In this instance, how a magnitude proportional to the time difference. If beacon A is being interrogated, the error . ever, it is preferred that the multivibrator be voltage is applied through operation of switch 6% to memory circuit A. As will be explained pres ently, memory circuit A produces an output volt age proportional to the range of beacon A. When beacon A is being interrogated, the output voltage supplied with a ?xed bias voltage. The ?xed bias is supplied so that the square voltage pulse produced by the multivibrator will have a con stant time width. Delay circuit as may be a uni-stable multivibrator or it may be an elec trical delay line. The beacon response or index of memory circuit A is applied through action of pulse is fed from receiver is to coincidence cir switch 588 and through line 59 to range delay cirw cuits ti and as. Coincidence circuits ti and t3 , cuit 5%. If memory circuit A is producing a volt~ 75 are arranged so that a pulse appears in the out 2,508,505 8 put'of these circuits only if the reference‘pulsc' . producing a delay in the reference pulse, said delay being of certain magnitudes when switches and the ?rst pulse of the beacon response ap 88 and 89 are in position “A" and being of other pears simultaneously therein. Coincidence cir cuits 8| and 03 are essentially ampli?ers having magnitudes when switches 98 and 99 are‘ in posi two signal inputs, In this respect they are some 5 tion "B," the magnitude of the various delays being adjustable by movement of contactors I02, what similar to audio frequency mixer circuits. However, they diner from thwe mixer circuits I03, I00,_and'l01. The, outputs of delay circuits 98 and 81 are in that the bias on both signal inputs is great fed to coincidence circuits H2 and II! respec enough to prevent .the generation of an output signal unless a signal is present at both signal 10 tively. The coincidence circuits H2 and III are inputs. Therefore, if the beacon response or in dex pulse arrives at a time directly between the gate pulse from generator 80 and the delayed gate pulse from circuit 82, equal pulses will be applied to di?erential error circuit 84 and no error voltage will be generated by the latter cir cuit. Ii’. however, the beacon response or index pulse occurs at a time more nearly coincident also supplied with the beacon response from the video circuit of receiver II and produce a pulse in their output, when the delayed reference pulse coincides in time with one o! the pulses in the coded series of the beacon response. The out ' puts of coincidence circuits H2 and H3 are ap plied to connector circuits III and II! respec— tively. Connector circuits H4 and H5 will allow the differential error voltage from circuit 84 to with the gate pulse from generator 80 then a larger pulse will be produced by coincidence cir 20 pass to the memory circuits A or B only when the reference pulse has been properly‘ delayed cuit 8I than is the case for coincidence circuit by circuits 96 and 91 to coincide with the coded 83 and an error voltage of one polarity will be series of beacon responses. produced. If the beacon response arrives at a When the antenna points toward beacon A, time more nearly coincident with the delayed gate pulse from generator 80, then coincidence 26 switches 98 and 99 will be shifted by member 33 of Fig. 1, into their A positions and the beacon circuit 83 will produce a larger pulse than will tracker circuit will then accept only responses coincidence circuit 8| and an error voltage of coded in accordance with the code of beacon A. opposite polarity will be generated by the latter circuit. Diiferential error circuit 84 which pro duces the error voltage is preferably a, type of diiierential ampli?er circuit followed by a low pass ?lter. The low pass ?lter in effect converts the pulses of error voltage coming from the dif ferential ampli?er into a steady or slowly chang ing error voltage. This steady or slowly chang ing voltage is essential to the proper operation of range delay circuit 58. The components of the circuit in Fig. 4 are constructed and operate in the manner set forth in the application by Andrew B. Jacobsen, Serial No. 584,233, referred to above. In the apparatus described above, reliance is placed on the directional qualities of antenna is for insurance that the proper beacons are be ing tracked. If additional insurance is required that the proper beacons are being tracked, the beacon tracking circuit may be arranged to ac cept responses’ from beacon A as identi?ed by the known coding of its pulses, when the antenna When antenna points toward beacon B. switches _ 30 98 and 99 will be shifted to the “B” position and beacon tracker 60 will accept only impulses coded in accordance with the code of beacon 2B. The components of the circuit in Fig. 5 may be similar in construction and operation to corre 35 sponding circuits described in the application by Andrew B. Jacobsen, Serial No. 584,233, referred to above. Each of memory circuits A and B may be con structed as set forth in Fig. 6. In Fig. 6, the sig 40 nal or error voltage is applied to terminal I08 and, during the duration of said error voltage, capacitors I69 and I10 charged with the charg ing current ?owing through resistor "I. The charge on capacitor I68, serving as bias for elec 45 tron tube I12, controls the amount of plate cur. rent ?owing through this tube and thus the amount of current through resistor I13. When the potential at the end of resistor I13 con nected to resistor I14 rises above the charge points toward beacon A, and to accept only pulses 50 on capacitor I10, current ?ows through resistor I14 to increase the charge on capacitor I10. from beacon B when the antenna points toward that beacon. Connected to‘the plate of tube I12 is shown a Referring now more particularly to Fig. 5 for source of voltage I 15. Switches I16, I11, and a tracking circuit capable of discriminating I18 are mechanically connected together and rep among coded responses, gate generator 90, co '55 resent a single throw triple-pole device which is normally open but when closed permits man incidence circuits BI and 98, delay circuit 92, and differential error circuit 04 are constructed ual setting of the bias supplied by connector 58 and operate in a manner similar to that set forth to range delay unit 58 by moving the sliding for components 80, 8I, 83, 82, and 84 respectively contact on potentiometer I19 which has con--‘ in Fig. 4. The reference pulse from range de 60 nected across its sources of voltage I80 anod I8I. , lay circuit 58 is also applied to delay circuits 96 The manner in which memory ‘circuits A and and 91. Delay circuits 96 and 91 are provided . B operate may be explained with reference to Fig‘. with ganged switches 88 and 99 respectively, each 6. The voltage charge across capacitor I69 is having left positions ,“A,” right positions “B,” proportional to the error voltage. If this is a and neutral positions “N.” In positions “A,” 65 large voltage, tube I12 conducts more readily switches 98 and 99 make contact with movable and the potential at terminal I82 will rise rap- , contactors I02 and I03 01' potentiometers ‘I04 idly. The potential at terminal I82 rises or falls and I05 respectively, said potentiometers being in an exponential manner due to the charge or connected between a source of positive'potential discharge of capacitor I10. The grid of tube and ground. In the “B” position, switches 98 and 70 I12 rises with the cathode as the grid is con 89 make connections with contactors I06 and I01 nected to the cathode by resistors HI and ‘I14 of potentiometers I08 and I09 respectively, said and capacitor I68. , . potentiometers each being connected between a Thus. it will be seen that a positive error volt source of positive potential and ground. Delay age applied at terminal I68 will produce an out’ circuits 96 and 91 may be any circuits capable of ‘"5 put voltage at terminal I82, said output voltage aso’acco increasing at a rate depending on the magnitude part of the distance comprising a potential sup= of the error voltage. A negative error signal at plied by either potentiometer d‘! or 48, which represents a measure of the major part of the referred to distance. A second means, range de terminal use will produce a. similarly decreasing output voltage. Said increase or decrease in out put voltage will continue for a time which is lay unit 58, is provided for additionally delay long compared to the interrogation period. ing the reference pulse, the purpose of which When switches H5, Ill and H8 are closed, resistor i'ié is shorted and it is possible to con trol the voltage at terminal 182 by regulating is to establish coincidence of the reference and the index pulses and is comprised of a bias or range potential which represents a measure of _ v potentiometer 5133. Switch I'll prevents power 10 the remaining part of the distance. A comparison circuit, the beacon tracker 68, losses from sources 1186 and it! when poten is provided for producing an error potential pro tiometer H9 is not being used. portional to the deviation from the aforemen The output of memory circuits A and B are applied as bias to range vdelay unit by means tioned coincidence which results from travel of of switch 63. 15 the craft. Memory circuits A and B each produce a volt-' Also, there is provided a memory circuit, the memory circuit A or B, comprising means for age bias indicative of the range to 2, correspond storing the range potential. This memory cir ing ?xed beacon. This range voltage initially out also includes means responsive to the error set or stored in the circuit by the manual op eration described above in locating the beacon 20 signal for adjusting the stored range potential in correspondence with the rate of change of and therefore varies in accordance with the er the range. ror voltage generated by unit to. If the beacon Also there is provided means, the potentiometer is interrogated intermittently, memory circuit 23 ?ll or potentiometer ‘H, for establishing a po develops a voltage between the replies, said volt age being indicative of the range determined by 25 tential representing a desired range for the par the last reply. ticular station and means, the meter 65 or 6t. Referring to Fig. 6, the rate at which capacitor for indicating the difference between the meas ured and desired range. lid changes its charge is proportional to the ve locity of the moving interrogator with respect While there has been described what is at to the beacon. The time constant of the cir 86 present considered to be the preferred embodi cuit containing capacitor l'l? is approximately ment of this invention. it will be obvious to those equal or larger than the longest time interval skilled in the art that various changes and modi= ?cations may be made therein without depart between successive appearances of the video sig nal permitting capacitor lid to change its volt ing from the scope of the invention as set forth age; thus, changing the bias on range delay unit 35 in the appended claims. The invention claimed is: 58 in relation to the rate of change of the dis 1. In a radio navigation system means for tance between the interrogator and the ?xed transmitting electromagnetic energy pulses and beacon which results in velocity memory. If the for receiving signals from each of a plurality rate of change of the distance between inter of remote sources responsive to said transmitted rogator and the beacon remains constant, the memory circuit will anticipate the change in pulses, means for generating a reference pulse distance between successive interrogations and each time a pulse is transmitted, ?rst predicting means providing a voltage the amplitude of which position the reference pulse so that it is coin is proportional to the anticipated time interval cident with the received reply or index pulse. Referring to Fig. 6, it will be noted that when 45 between the time of occurrence of said refer switches fit, if? and We are closed the voltage ence pulses and the time that signals from a at terminal I82 may be controlled manually to first remote source are received, second predict ing means providing a. voltage proportional to adjust the delay of unit 58 to position the ref the anticipated time interval between the time erence pulse output of 5% at coincidence with the received pulses, thus permitting a particular bea '50 of occurrence of said reference pulses and the con to be searched for and, after ?nding the time signals from a second remote source are received, delay means responsive to said pre beacon, the opening of switches 178, ill, and dicting means for delaying said reference pulses, 978 will permit the beacon to be tracked auto matically, ?rst switch means having at least two opera From the description given above, it will be 55 tive positions, said switch means connecting said ?rst predicting means to said delay means when clear that in accordance with the present in .in a ?rst operative position and connecting said vention, there is provided a navigation system for continuously determining the location of a second predicting means to said delay means when in a second operative position, a comparison mobile craft relative to a plurality of fixed sta tions located at known positions comprising 60 circuit responsive to said delayed reference pulses means for establishing communication periodi and signals from said remote sources, said com parison circuit providing an error signal propor cally between the craft and each of these sta~ tions. ' tional to the time interval between the time of ‘occurrence of said delayed reference pulse and Also there is provided the means, timer H for producing at the craft a timing and a reference the time that said signals are received, second switch means having at least two operative posi pulse recurrent at a chosen repetition rate and tions, said second switch means connecting said means, receiver 58, responsive to the commu comparison circuit to said ?rst predicting means nication with a particular one of these stations when in a ?rst operative position and to said sec for producing an index pulse having a time delay relative to the reference pulse which corresponds 70 ond predicting means when in a second operative position; and means for causing said ?rst and sec to the distance of the craft from the particular ond switch means. to be in said first operative pom station. ' sition's when signals from said ?rst source are Also, there is provided a ?rst means, the step delay unit 66, for delaying ‘the reference pulse ' being received and in said second operative po by an amount corresponding to a chosen major 75 sltion when signals from said second source are 3,608,600 .11 v , being received whereby the signal from said com parison means controls the output of said pre dicting means‘so that errors, if any, between said anticipated time intervals and the actual time intervals between the time of occurrence of said reference pulses andthe time said signals _ are received from said remote sources are sub stantially eliminated. 12 , storage means thereby storing data - only one of said sources. relative to 7. A navigation system for continuously de termining the location of a mobile craft‘rela tive to a plurality of ?xed stations located at known positions comprising means for establish ing communication cyclically between said craft and each of said stations, means for producing 2. Apparatus as claimed in claim 1 wherein at said craft a timing and a reference pulse re said comparison circuit includes means for re 10 current at a chosen repetition rate, means re jecting received signals not having a predeter sponsive in turn to the communication with each mined code. one of said stations for producing in turn an 3. Apparatus as claimed in claim 1 said ap index pulse having a time delay relative to said paratus further comprising means for establish reference pulse which corresponds in turn to ing a ?rst ?xed reference voltage, means for 15 the distance of said craft from each of said comparing the output of said ?rst predicting stations, a ?rst means for cyclically delaying means with said ?rst reference voltage and in said reference pulse by an amount which in turn dicating the di?erence in amplitude if any there corresponds to a chosen major part of said dis between, means tor estabishing a, second ?xed tance from each of said stations comprising a plu- ' ‘reference voltage, and means for comparing the 20 rality of potentials which represent in each case output of said second predicting‘means and in dicating the difference, if any, therebetween. 4. A system for tracking a plurality of signals the measure of said major part, a second means for additionally delaying said reference pulse by an amount which corresponds in each case to the remaining part of said range, to establish co prising means for generating a reference pulse, 25 incidence of said reference and said index pulses, delay means responsive to an input bias voltage comprising a bias or range potential which rep for delaying said reference pulse, ‘a comparison resents a measure of the remaining part of said circuit for generating an error voltage propor range, a comparison circuit for producing an tional to the time spacing between said delayed error potential proportional to the deviation from reference pulse and a received signal, a plurality 30 coincidence which results from travel of said ' of signal storage means, a ?rst switch means craft, a corresponding plurality of memory cir having a plurality of operative positions, each cuits comprising means for storing said range of said positions selectively connecting said com potentials which represent the range of each of parlson circuit to one of said signal storage said stations and means responsive to said error means, a second switch means having a plu signal for adjusting each of said stored range ‘rality of operative positions, each of said op potentials in correspondence with the rate of erative positions connecting said delay means to change of said range, means ior establishing a one of said signal storage means and means for corresponding plurality of potentials, each rep- ' causing said ?rst and second switch means to as resenting the desired remaining part of said range sume predetermined operative positions as each and means for indicating in each case the dif signal is being received whereby the output of ference between said measured and said desired range. said signal storage means acts as the input bias voltage to said delay means and said error signal 8. A navigation system for continuously de causes the output of said signal from said signal termining the location of a mobile craft relative 45 storage means to change in a direction that to a plurality of ?xed stations located at known will reduce the amplitude of said error signal, positions comprising, means for establishing com the output signal from each of said storage means munication periodically ‘between said craft and thereby providing a measure of the time interval each of said stations, means for producing at between the time a pulse-is transmitted and the said craft a timing and a reference pulse re~ 50 current at a chosen repetition rate, means re time a particular signal is received. 5. Apparatus as claimed in claim 4 wherein sponsive to the communication with a particular said delay means comprises two serially connected one of said stations for producing an index pulse delay circuits, one of saidv circuits being respon having a time delay relative to said reference sive to the bias voltage supplied from said storage pulse which corresponds to the distance of said means and the other of said delay circuits being craft from said station, a ?rst means for delay responsive to a second input bias voltage, said ing said reference pulse by an amount correspond apparatus further comprising a plurality of ad ing to a chosen major .part of said distance com prising a potential which represents a measure .iustable bias sources, a third switch means hav ing a .plurality of operative positions, each of of said major part, a second meansi'or addition. received in response to a transmitted signal com‘ said positions connecting said other delay cir 60 ally delaying said reference pulse to establish cuit to one of said adjustable bias sources, and coincidence of said reference and said' index means for operating said third switch means in synchronism with said ?rst and second switch pulses, comprising a bias or range potential which represents a measure of the remaining part of means. said distance, a comparison circuit for produc 6. In a range tracking system wherein signals 65 ing an error potential proportional to the devia from a plurality of sources are intermittently tion from said coincidence which results from received, and wherein said range tracking sys travel of said craft, a memory circuit compris tem comprises means for generating energy rep _ ing means for storing said range potential, means resenting a, characteristic of each of said sig responsive to said error signal for adjusting said nals, and means for storing said energy, means 70 stored range potential in correspondence with for simultaneously tracking a plurality of sig the rate of change of said range, means for nals comprising a plurality of said storage means establishing a potential representing a desired and switch means for connecting a different range for said particular station and means for storage means to said generating means each indicating the difference between said measured, time a different signal is received, each of said 75 and said desired range. a 9. A navigation system for continuously de lishing communication periodically between said termining the location of ‘a mobile craft rela tive to a plurality of ?xed stations located at known positions comprising, means for estab craft and each of said stations, means for pro ducing at said craft a timing and a reference pulse recurrent at a chosen repetition rate, means lishing communication periodically between said responsive to the communication with a par?‘ craft and each of said stations, means for pro ducing at said craft a timing and a reference ticular one of said stations for producing an index pulse having a time delay relative to said pulse recurrent at a chosen repetition rate, means reference .pulse which corresponds to the range responsive to the communication with a parof said craft from said station, means for de ticular one of said stations for producing an in 10 laying said reference pulse by an amount which corresponds to said range, to establish coinci dex pulse having a time delay relative to said dence of said reference and said index pulses, reierencekpulse which corresponds to the range comprising a bias or range potential which rep-, of said craft from said station, means for de resents a measure of said range, a comparison laying said reference pulse by an amount which corresponds to said range, to establish coinci 15 circuit for producing an error potential propor tional to the deviation from coincidence which dence of said reference and said index pulses, comprising a bias or range potential which rep results from travel of said craft, a memory cir cuit comprising means for storing said range resents a measure of said range, a comparison circuit for producing an error potential propor potential, for adjusting means saidresponsive stored range to said potential errorin cor tional to the deviation from coincidence which 20 respondence with the rate of change of said results from travel of said craft, a memory cir range. cult comprising means for storing said range potential, means responsive to said error signal for adjusting said stored range potential in cor respondence with the rate of change of said 25 REFERENCES CHTED range, means for establishing a potential rep The following references are of record in the resenting a desired range for said particular ?le of this patent: station and means for indicating ‘the di?erence , UNITED STATES PATENTS between said measured and said desired range. 10. A navigation system for continuously de 30 Number Name Date the location of a mobile craft rela= 2,252,083 Luck ___________ _. Aug. 12, 19M tive to a plurality of ?xed stations located at w‘... a 2,307,029 M‘. ____________ .._ Jan. 5, 13 positions comprising, means for estab~
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