Patent Abstract:
A safety system for deterring a homing missile from attacking its launchingehicle whereby the launching vessel is enabled to alter the course and neutralize the detonator of the weapon.

Full Description:
BACKGROUND OF THE INVENTION 
     The present invention relates to homing missiles, and more particularly, to a turnaway and dudding deterrent to an accidental attack by a weapon on its launching vessel. 
     In homing weapons, a search and acquisition system examines the surrounding environment, usually by acoustic or electronic means, for noise emanating from or, for other signs indicative of, the presence of a target. When first launched, the immediate proximity of the launching vehicle and the amplitude of its attendant noise shadow the presence of the target and increase the risk that the weapon&#39;s search system will acquire and return to the launching vehicle. Consequently, the weapon&#39;s search and acquisition system can not be activated until the weapon has traveled a predetermined distance (i.e., cleared the activation zone) from the launching vehicle. 
     Variable propagation conditions, quieting trends in vessel construction as well as mere quiescence, however, frequently mask the presence of a target until it is at close quarters with the launching vessel, often inside or just outside the activation zone. In these situations, as the azimuth, depth and range of the target is seldom immediately ascertainable, a vessel-to-vessel weapon must be capable of, on sudden launching, searching for and acquiring a vagariously moveable target at close quarters without endangering the launching vessel. Prior art weapon safety systems protect the launching vessel from an undesired attack by its own weapon by controlling activation and operation of the weapon&#39;s search and acquisition system. The weapon&#39;s system is not activated until the weapon has cleared a volume surrounding the launching vessel that can be best described as a spheroid having a semiaxis approximately colinear with the major axis of the launching vessel (i.e., a protective zone). If the weapon re-enters the spheroid, its system is deactivated. When the weapon is outside of the spheroid, its system is limited in its search to a lunular segment of a sphere. When launched against a target at close quarters with the launching vessel, a weapon having a prior art safety system has little or no opportunity for search and acquisition of the target. 
     SUMMARY OF THE INVENTION 
     The present invention overcomes the disadvantages, inconveniences and limitations of the prior art by providing a novel safety system for deterring a weapon from acquiring, homing on and attacking its launching vehicle whereby the weapon&#39;s guidance system is given greater opportunity for search and acquisition at close quarters when launched against a target having an unknown position and a capability for vagarious movement. Embodiments of the present invention use a tracking circuit for locating and following a weapon, a turnaway circuit for altering the course of a weapon that is homing on its launching vessel, and a dudding circuit for neutralizing the detonator of a weapon that has returned to within a preselected distance of the launching vessel, to provide adequate opportunity for search and acquisition of the target. A weapon so equipped may begin its search for a vagariously moveable target while in close linear proximity with its launching vehicle. 
     An object of the present invention is to provide a means for deterring a returning weapon from attacking its launching vehicle. 
     Another object of the present invention is to provide a safety system for deterring a returning weapon from attacking its launching vehicle whereby a weapon launched at close quarters against a vagariously moveable target will have adequate opportunity to search for and acquire the target. 
     Yet another object of the present invention is to provide a safety system whereby the course of a returning weapon may be altered without interrupting the operation of the weapon&#39;s search and acquisition system. 
     Still another object of the present invention is to provide a safety system whereby the detonator of a returning warhead may be neutralized without interrupting the operation of the weapon&#39;s search and acquisition system. 
     Still yet another object of the present invention is to provide a safety system for deterring a weapon from attacking its launching vessel, that is adaptable to prior art search and acquisition sytems. 
    
    
     BRIEF DESCRIPTION OF THE DRAWINGS 
     A more complete appreciation of this invention and many of the attendant advantages thereof will be readily appreciated as the same becomes better understood by reference to the following detailed description when considered in connection with the accompanying drawings wherein: 
     FIG. 1 is a geometric diagram of the relative positions of the transducers used in the circuits of embodiments of the invention; 
     FIG. 2 is a block diagram of a weapon safety system according to the invention. 
     FIG. 3 is a repetition of the geometric diagram of FIG. 1 reduced in scale in order to show the threshold condition. 
     FIG. 4 is a partially cut-away drawing illustrating the installation of a pair of electrodes on the hull of a submarine. 
    
    
     DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT 
     Referring now to the drawings wherein like reference characters designate identical or corresponding parts throughout the several views, and more particularly, to FIG. 1 wherein a set of three Cartesian coordinates is superimposed on a point source spatial representation of the transponder of a weapon, point T, and the hydrophones of its launching vessel, points P 1 , P 2 , P 3  P k . At least three antennae, such as hydrophones, are mounted in a non-colinear array on the launching vessel. After the weapon has been launched, one of the hydrophones mounted on the launching vessel issues an acoustic pulse. The weapon transponder receives the pulse and within a short time transmits a return pulse. Using classical rangefinding techniques, the distance R x  between any hydrophone and the weapon transponder located at point T is proportional to the time &#34;t&#34; lapsing between transmission of the pulse and receipt of the return pulse according to the formula: ##EQU1## 
     The variable &#34;c&#34; is the speed of sound in the surrounding medium. Accordingly, the distances between hydrophones located at P 1 , P 2  and P 3  and the transponder located at point T, respectively, R 1 , R 2  and R 3 , are readily ascertainable. Then, three of the hydrophones that have received the return pulse, perhaps those located at points P 1 , P 2  and P 3 , are taken as defining an X-Y plane. The distances between points P 1  and P 2 , P 2  and P 3 , and P 1  and P 3  are the known values D 1 , D 2  and D 3 , respectively. By simultaneously solving the equations of three spheres with centers at P 1 , P 2  and P 3 , respectively: 
     
         x.sup.2 +y.sup.2 +z.sup.2 =R.sub.1.sup.2                   (2) 
    
     
         (D.sub.1 -x).sup.2 +y.sup.2 +z.sup.2 =R.sub.2.sup.2        (3) 
    
     
         x.sup.2 +(D.sub.3 -y).sup.2 +z.sup.2 =R.sub.3.sup.2        (4) 
    
     the x, y and z coordinates, and thus the location of point T, may be determined. 
     After each pulse is received, and the interval of time between transmission and reception for each hydrophone is noted, another pulse is transmitted and the process is repeated, thereby enabling the launching vessel to continuously track the weapon&#39;s progress. 
     FIG. 2 sets forth in a block diagram the interconnections between the various components of the weapon tracking circuit, the weapon turn-away circuit, and the weapon dudding circuit. Hydrophones 11, 12, 13 . . . k are mounted on the launching vessel in a non-colinear array and connected in separate channels through the switching transmit-receive network 20 and the receivers 30. 
     A preselected interval after launching of a weapon, computer 70 notes the time shown by clock 72 and sends a start signal over line 36 to transmitter 32 and timers 42, 46, 50. Upon receipt of the start signal timers 42, 46, 50 assume an ON state. Simultaneously, transmitter 32 generates an acoustic signal via switching transmit-receive network 20 and transducer 22. Switching transmit-receive network controls the connection of hydrophones 11, 12, 13 to receiver 30 so as to prevent reception during transmission. After receiving the acoustic signal, the weapon transponder (not shown) transmits a return acoustic signal. The return signal is received by hydrophone 11, connected via switching network 20 to and detected by one channel of receiver 30. Logic devices 40, 44, 48 are individually connected in series between timers 42,46, 50 respectively, and a corresponding channel of receiver 30. Upon detection of a return signal, receiver 30 generates a signal that switches logic device 40 to its ON state, thereby causing timer 42 to cease generation of periodic pulses. Timers 42, 46, 50 . . . n mark the transient time of the acoustic signal as it travels between transducer 22 and the corresponding hydrophone 11, 12, 13, . . . k. Input selector 60 senses the cessation of periodic pulses by timer circuit 42, transmits a pulse to time register 62, and conveys data to computer 70 indicative of the time at which timer 42 ceased generating. Time register 62 and computer 70 reference the pulse with the time shown by clocks 64 and 72, respectively. Ultimately, the return acoustic signal is individually received by hydrophones 12, 13, detected by the corresponding channels of receiver 30, thereby switching the corresponding logic devices, 44, 48 to their ONE states. 
     As each of the timers 46, 50 ceases generation of periodic pulses in response to the corresponding logic device being switched to its ON state, input selector 60 transmits a pulse to time-register 62 and computer 70, both of which reference their reception of the pulse with the time shown by clocks 64 and 72 respectively. 
     Upon receipt of the third set of data provided by input selector 60, computer 70 first calculates the corresponding distances R x  according to formula (1), and then calculates the coordinates of the weapon transponder according to formulae (2), (3) and (4) 
     After receiving the data transmitted by input selector 60, computer 70 generates a clear signal over line 34 in order to ground the channels of receiver 30 and to switch logic devices 40, 44,48 to their ZERO logic state. Computer 70 then notes the time shown by clock 72 and sends start signal over line 36, thereby reinitiating the tracking process. 
     By comparison with previously calculated coordinates, computer 70 is able to track the course of the weapon transponder. If computer 70 determines that the weapon transponder has reentered the protective zone on a course homing on the launching vessel, it causes transmitter 32 to generate a coded acoustic signal via transducer 22. Upon receipt of the coded acoustic signal by the weapon transponder, the weapon, alters its course and resumes search for a target in a sector other than that in which it acquired the launching vessel. 
     There are several sources of possible error in determining the true position and tracking the course of a weapon with respect to its launching vessel. The embodiment shown in FIG. 2 provides a second safety system, available if the weapon penetrates a second or neutralization zone encompassed by the activation zone (e.g., the turnaway safety system fails, or, the turnaway system performs but the weapon quickly resumes a course approximately homing on the launching vessel, thus indicating that the weapon must pass close by the launching vessel in order to reach the target). Upon making a determination that the weapon is within the activation zone Z 2 , (shown in the three dimensional Cartesian graph of FIG. 3) and maintaining a course approximately homing on the launching vessel, computer 70 causes electromagnetic generator 74 to create a magnetic field substantially corresponding to the neutralization zone via a plurality of electrodes 76 mounted on the launching vessel 100, as shown by the illustration of FIG. 4. As it enters the neutralization zone, electrodes 76 mounted on the weapon sense the magnetic field and cause the weapon detonator to be neutralized. Once clear of the neutralization zone, the weapon&#39;s detonator is again activated. 
     It will be apparent that the invention in the above described system discloses a method and apparatus enabling a vehicle to launch a weapon against a target at close quarters without unduly exposing itself to the risk of attack by a weapon that subsequently acquires and homes on the launching vehicle. By tracking its weapon, and utilizing the turnaway and dudding systems in accordance with the teachings of the present invention, a vehicle is enabled to launch a weapon capable of searching for and acquiring a target while still within the immediate vacinity of the launching vehicle. In addition, the dudding system provides safety for the launching vessel while a returning missile passes through the immediate vacinity of the vessel without interrupting the search and acquisition activities of the missile. 
     The foregoing embodiment is merely illustrative of the basic principles of the invention. Obviously, numerous modifications, variations and applications of the present invention are possible in the light of the above teachings. For example, although the weapon tracking system is described as having three tracking channels, it is possible for embodiments of the invention to have more than three channels, each channel having a hydrophone k individually connectable in series with one channel of a receiver 30, a logic device m and a timer n. In an embodiment having more than three channels, upon receipt and detection of a fourth return acoustic signal, respectively by hydrophone k and the corresponding channel of receiver 30, logic device m will be switched to its ON state thereby stopping timer n. Input selector 60, sensing that the timer n has ceased generation of periodic pulses, transmits a fourth pulse to time-register 62 and then covers data indicative of the time and identity of timer n to computer 70. Upon receipt of this data, computer 70 determines the value of the corresponding distance R x  according to formula (1) and then redundantly calculates and selectively compares the coordinates of the missile transponder. 
     While hydrophones 11, 12, 13 . . . k are selected for detection of a narrow range of acoustic frequencies in a seawater environment, in another embodiment, they might be replaced by another type of antenna or selected for detection of an above sonic range of frequencies. Although FIG. 2 shows clocks 64 and 72, a simplified embodiment constructed according to the invention could use a single clock for providing the time to both time register 62 and computer 70. 
     For the purpose of disclosing the present invention, the apparatus and method were described by reference to an embodiment used in a vessel for deterring a weapon from acquiring and attacking its launching vessel. It will be obvious to those skilled in the art that these teachings are equally applicable to a safety system for deterring a missile from detrimentally returning to any launching device, whether a mobile launching vehicle such as an aircraft, a land vehicle, a ship, a submersible, or a stationary launching assembly. 
     It is therefore to be understood that within the scope of the appended claims, the invention may be practiced otherwise than as specifically described.

Technology Classification (CPC): 5