US3739153A - Weapon firing computer - Google Patents

Weapon firing computer Download PDF

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Publication number
US3739153A
US3739153A US00171055A US3739153DA US3739153A US 3739153 A US3739153 A US 3739153A US 00171055 A US00171055 A US 00171055A US 3739153D A US3739153D A US 3739153DA US 3739153 A US3739153 A US 3739153A
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Prior art keywords
weapon
target
signal
potentiometer
grid
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US00171055A
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L Kendy
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Raytheon Co
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Hughes Aircraft Co
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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G5/00—Elevating or traversing control systems for guns
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G3/00—Aiming or laying means
    • F41G3/14—Indirect aiming means
    • G—PHYSICS
    • G06—COMPUTING OR CALCULATING; COUNTING
    • G06G—ANALOGUE COMPUTERS
    • G06G7/00—Devices in which the computing operation is performed by varying electric or magnetic quantities
    • G06G7/48—Analogue computers for specific processes, systems or devices, e.g. simulators
    • G06G7/80—Analogue computers for specific processes, systems or devices, e.g. simulators for gunlaying; for bomb aiming; for guiding missiles

Definitions

  • the present invention is a fire control computer which 235/189 computes weapon firing data from known information [51] Int Cl G06 7/80 set into the computer by handset controls in a predeter- [58] Fieid 5 B mined sequence of operations.
  • the fire control com- 235/61 5 E 189 i puter is analog in nature and uses handset knobs and switches coupled to dials to input known information [56] References Cited to potentiometers and resolvers'.
  • the gunnery problem is primarily the problem of indirect fire.
  • the solution of this problem requires weapon and ammunition settings which, when applied to the piece and the ammunition, will cause the projectile to burst on, or at a proper height above, the target.
  • the steps in the solution of the gunnery problem are a. Location of the target and battery,
  • Weapon firing is accomplished by a team effort.
  • the elements of the gunnery team are a.
  • Observers The observers (to include all target acquisition devices) detect and report to the fire direction center the location of suitable targets, initiate calls for fire, and conduct an adjustment if necessary.
  • the fire direction center evaluates the information received from the observers, determines firing data, and furnishes these data in the form of fire commands to the firing battery.
  • the firing battery applies the firing data to the weapons and fires the weapons.
  • the prior art methods of computing the firing data vary depending on the type of weapon. For example, for field artillary the computation is usually provided by a digital computer. On the other hand, when mortars are being fired, the computations are made by graphical techniques and hand computations using a plotting board, special scales, slide rules, nomographs, charts and tables. In the event of a failure in a field artillery digital computer, the backup computations are performed in the same manner as for the mortars. Hand computations are subject to human error, especially because many different scales and tables must be read and geometric constructions must be made. In addition, considerable training time and skilled personnel are required.
  • the invention provides a primary means of computing mortar firing data in a manner suitable for use by personnel having a minimum of training, and a backup means of computing field artillery firing data.
  • the present invention is a fire control computer which computes weapon firing data from known information set into the computer by handset controls in a predetermined sequence of operations.
  • the fire control computer is analog in nature and uses handset knobs and switches coupled to dials to input known information to potentiometers and resolvers. Other knobs and switches are used to null electrical signals to resolvers and potentiometers to provide the desired information on dials which may be read by the operator.
  • FIG. 1 is a diagram of a typical grid coordinate system used for weapon firing.
  • FIG. 2A is a portion of the circuit diagram common to both of the alternate preferred embodiments of the present invention shown in FIGS. 28 and 2C.
  • FIG. 2B is a portion of the circuit diagram for one preferred embodiment of the present invention.
  • FIG. 2C is a portion of the circuit diagram for a second preferred embodiment of the present invention.
  • FIG. 3 is a diagram of an operators panel for the present invention.
  • FIG. 1 there is shown a typical grid coordinate system used for weapon firing.
  • the grid coordinates will be on a map of the area.
  • the weapon will be in a position on the grid coordinate system identified by the distance in meters along the grid east coordinate E and the distance in meters along the grid north coordinate N
  • the observer will be at a position identified by the distance in meters along the grid east coordinate E and the distance in meters along the grid north coordinate N
  • the target will be at a position identified by the distance in meters along the grid east coordinate E and the distance in meters along the grid north coordinate N
  • the information required for firing the weapon is the direction from the weapon to the target measured as an angle from the grid north coordinate to the straight line drawn between the weapon and the target.
  • the angles for weapon firing are measured in mils. An angle of 1 mil will subtend an arc of 1 meter at a distance of 1,000 meters.
  • the angle of elevation and the charge is a function of the range R from the weapon to the target. If the grid positions of the weapon and the target are known, the direction angle 0 and the range R may be obtained in a fairly straightforward manner by solving the following equations:
  • the computations become increasingly difficult. For example, many times the grid coordinate position of the target is unknown. Furthermore, the weapon firing personnel may not be able to see the target and thus would not have any way of determining the range or the direction angle from the weapon to the target. Thus, in many types of weapon firing, an observer located at a point distant from the weapon position may make estimates of the direction angle B from the observer to the target and the range R from the observer to the target. This information is transmitted to the weapons firing personnel. Then, if the grid position E and N of the observer is known, the direction angle 0 and the range R from the weapon to the target may be determined by trigonometric relationships. It should be apparent that the trigonometric computation would be fairly complex. Additional complications are brought in by the fact that many times the grid position of the observer is not known. In any case, if a certain minimum amount of information is known, it may be possible to compute by actual computation or geometric constructions or table lookup procedures the weapon firing information needed.
  • FIGS. 2A and 2B show a circuit diagram for one embodiment of the weapon fire control computer of the present invention.
  • power for the circuitry is supplied by batteries 10.
  • the direct current from the batteries is coupled through a push-toclose power switch 12 to a solid state inverter 14 which provides an alternating current output when the switch 12 is closed.
  • the output of the solid state inverter 14 is coupled to the primary coil of a transformer 16.
  • the transformer 16 will have secondary coils to provide the required voltages for the operation of the circuitry.
  • the terminals P1, P2, P3, P4, P5 and P6 correspond to similarly labelled terminals in the remainder of the circuit diagrams where the voltage on the transformer terminal is applied.
  • the circuitry shown in FIG. 2A further includes a potentiometer 20 which represents the algebraic difference between the observer's grid east coordinate and the weapon grid east coordinate (E E The potentiometer 20 is positioned by handset knob S4.
  • a potentiometer 22 is provided to represent the algebraic difference between the observer's grid north coordinate and the weapon grid north coordinate (N N The potentiometer 22 is positioned by handset knob S5.
  • a potentiometer 24 represents the algebraic difference between the target grid east coordinate and the weapon grid east coordinate (E E The potentiometer 24 is positioned by handset knob $10.
  • a potentiometer 26 represents the algebraic difference between the target grid north coordinate and the weapon grid north coordinate (N N The potentiometer 26 is positioned by handset knob S11.
  • a potentiometer 28 is provided to represent the range from the observer to the target R
  • the potentiometer 28 is positioned by handset knob S3.
  • the output of the potentiometer 28 is applied to one of the rotor windings of a resolver 30.
  • the second rotor winding of the resolver 30 is coupled to ground potential.
  • the rotor of the resolver 30 is positioned by handset knob S2.
  • the angular displacement of the knob S2 is representative of the direction angle from the observer to the target 0
  • a first stator winding 32 of the resolver 30 provides an output which is representative of the function R sin G
  • a second stator winding 34 provides an output which is representative of the function R cos 0
  • the first stator winding 32 of the resolver 30 is coupled to one input of a summingjunction 36.
  • the output of the potentiometer 20 is coupled to a second input of the summing junction 36.
  • One output of the summing junction 36 is coupled to a contact for position (d) of a first pole of a multipole-multiposition selector switch S1.
  • a second output of the summingjunction 36 is coupled to a contact (a) of a double pole/double throw switch S6.
  • the output of the potentiometer 24 is coupled to a contact (b') of the switch S6.
  • a pole terminal (c') of the switch S6 is coupled to a first stator winding
  • the second stator winding 34 of the resolver 30 is coupled to a first input of a summing junction 42.
  • the output of the potentiometer 22 is coupled to a second input to the summing junction 42.
  • One output of the summing junction is coupled to a contact for position (e) of the selector switch S1.
  • a second output of the summing junction 42 is coupled to a contact (a) of the double pole/double throw switch S6.
  • the output of the potentiometer 26 is coupled to a contact (b) of the switch S6.
  • a pole contact (c) of the switch S6 is coupled to a second stator winding 44 of the resolver 40.
  • the rotor of the resolver 40 is positioned by handset knob S12.
  • the angular position of the knob S12 is representative of the direction angle from the weapon to the target 0
  • a first rotor winding 46 of the resolver 40 is coupled to a second pole of the switch S1 identified as S1.
  • a second rotor winding 48 of the resolver 40 is coupled to one input of a summing junction 50, to a third pole of the switch S1 identified as S1" and to one input of a divder circuit 64.
  • the output of a potentiometer 52 is coupled to an input of the summing junction 50.
  • the potentiometer 52 is positioned by handset knob S14.
  • the output of the potentiometer 52 is representative of the range from the weapon to the target R
  • the output of the potentiometer 52 is also coupled to the contacts representative of positions (d) and (e) of the third pole S1" of switch S1.
  • the output of the summing junction 50 is coupled to a contact representative of position (b) of switch S1.
  • the first condition to be described is that where the target grid coordinates are known and the weapon grid coordinates are known.
  • Switch S6 is put into position (b).
  • the potentiometer 24 is set by knob S10 to the algebraic difference between the target grid east coordinate and the weapon grid east coordinate (E E )
  • the potentiometer 26 is set by knob S11 to the algebraic difference between the known target grid coordinate and the weapon grid north coordinate (N N).
  • the voltage representative of E E is applied to stator winding 38 of the resolver 40.
  • the voltage representative of N N is applied to the stator winding 44 of the resolver 40.
  • Switch S1 is placed in position (a).
  • the second set of contacts S1 for the switch S1 will couple the first rotor winding 46 of the resolver 40 through a summingjunction 60, which will be ignored for the present, to contact (a) of the first set of contacts for switch S1.
  • the pole of switch S1 is coupled to a voltmeter 56 adapted to act as a null meter. With power switch 12 held in the closed position, the knob S12 is rotated until the voltage output on the first rotor winding 46 goes to zero as shown by the voltmeter 56. The position of the knob S12 then represents the direction angle from the weapon to the target 0 This angle 0 may then be read from a counter coupled to the knob S12 and calibrated to read in military mils.
  • the switch S1 is placed in position (b).
  • the switches indicated as S1 and S1" will not electrically change from the position shown in FIG. 2B.
  • the second rotor winding 48 will have an output voltage as a result of the prior setting of the resolver by knob S12. This output voltage is coupled to the summing junction 50.
  • the third input to the summing junction 50 will be ignored for the present.
  • the output of the summingjunction 50 is coupled to position (b) of switch S1. Voltage is then applied to the voltmeter 56.
  • knob S14 is rotated until the output voltage from the potentiometer 52 applied to the summing junction 50 balances the voltage from the second rotor winding 48 from the resolver 40 as shown by the voltmeter 56. When the voltages are balanced, the knob S14 position will indicate the range from the weapon to the target R This range may then be read from an indicator which may be calibrated in meters.
  • the weapon grid coordinates may be known but the target grid coordinates will not be known and the target cannot be seen by the weapon firing personnel.
  • an observer located at some position distant from the target and the weapon is used to provide weapon firing information.
  • the weapon grid coordinates are known and the observer grid coordinates are known.
  • E E is set on potentiometer by knob S4.
  • N N is set on potemntiometer 22 by knob S5.
  • Switch S6 is placed in position (a).
  • the observer will sight on the target to provide an estimate of the direction angle from the observer to the target 0 and an estimate of the range from the observer to the target R
  • the direction angle 0 is set on knob S2 which rotates the rotor of the resolver 30.
  • the range R is set on knob S3 which sets potentiometer 28 to give a signal representative of the value of the range R
  • the first stator winding 32 of the resolver 30 will provide an output signal representative of R sin 0
  • This signal is applied to the summing junction 36 where it is summed with the signal from the potentiometer 20 which is representative of E E
  • the output of the summing junction 36 will then provide a signal which is representative of E E in accordance with the following equation:
  • contact (0') of switch S6 will provide a signal representative of the target grid east coordinate with the offset for the weapon grid east coordinate.
  • contact (c) of switch S6 will provide a signal representative of the target grid north coordinate with an offset for the weapon grid north coordinate.
  • the weapon grid coordinates may be known but the target grid coordinates are not known and the observer grid coordinates are not known. Before the observer can provide meaningful data regarding the position of the target, the observers grid coordinates must be known.
  • the circuitry of the present invention provides a means for providing this information. Assuming now that the observer can see the weapon position, one method of locating the observers grid coordinates is to have the observer sight on the weapon and provide information regarding the direction angle from the observer to the weapon and the range from the observer to the weapon. This information is set on knob S2 and knob S3. Knobs S12 and S14 are set to zero. Switch S1 is set to position (d) or position (e).
  • switch S1 With switch S1 in position ((1) or (e), the set of contacts labeled S1 will provide a ground signal to the first rotor winding 46 of the resolver 40. In a similar manner, since knob S14 is set to zero (ground), the switch contact labeled S1" will provide a ground signal to the second rotor winding 48 of the resolver 40. Further, since knob S12 is at zero, the stator windings 38 and 44 of the resolver 40 will be at ground. Switch S6 is set to position (a) and ground will be applied to summing junctions 36 and 42. Now, with switch S1 in position (d), and switch 12 depressed, the output of the summing junction 36 is applied to the voltmeter 56.
  • knob S4 is rotated until the voltmeter is nulled with the signal from the stator winding 32 of resolver 30.
  • the potentiometer 20 will then be set to the observer grid east coordinate with the offset for the weapon g'rid east coordinate in accordance with the following equation:
  • the observer may then provide information concerning target location and firing information may be determined as previously described.
  • Another method of determining the observer grid position is to set in target grid position east and north on knobs S10 and S11. Then with switch S6 in position (b), weapon firing information O and R is determined with knobs S12 and S14 following the procedure described previously. Now, the observer may sight on the known target and give the direction angle and range from the observer to the target 9 and R If there is no known target, the weapon firing personnel may fire a marking round with the firing information previously determined. The observer then sights on the burst of 7 the marking round and gives his direction angle and range information. This information is set on knobs S2 and S3. Switch S6 is then placed in position (a) and switch S1 is placed in position ((1) or (e). Knobs S4 and S5 are then used to null the signals. The potentiometers 20 and 22 will then provide signals representative of the observer grid east coordinate offset for the weapon grid east coordinate and the observer grid north coordinate offset for the weapon grid north coordinate respectively.
  • knob S12 Under normal conditions without a direction adjustment, knob S12 would be rotated until the signal on rotor winding 46 of the resolver 40 is zero.
  • a summing junction 60 is provided to accept the signal from switch contact S1 for positions (a), (b) and (c). The output of summing junction 60 is coupled to position (a) of switch S1.
  • a potentiometer 62 is provided to give a positive or negative direction adjust signal. The potentiometer 62 is operated by knob S7. The output of the potentiometer 62 is applied to a divider circuit 64.
  • the signal on rotor winding 48 is coupled to one input to the divider 64.
  • the fixed voltage from the potentiometer 62 is coupled to the other input to the divider 64.
  • the signal from the potentiometer 62 is then sealed to be proportional to the resolver excitation.
  • the divider output is coupled to the summing junction to provide the adjustment for the fixed angle bias.
  • switch S6 is set to position (b).
  • Knobs S10 and S1 1 are set to the known target grid coordinates used for the registration.
  • Knobs S12 and S14 are left at the positions finally determined by the registration.
  • Switch S1 is set to position (a) and the input to voltmeter 56 is nulled by adjusting potentiometer 62 with knob S7.
  • the range adjustment for the registration firing is proportional to the error for the registration round.
  • This adjustment can be accomplished by changing the scale factor of the potentiometer 52 which represents the range from the weapon to the target.
  • the scale factor adjustment is made by using an additional potentiometer 58 which is operated by knob S8.
  • the output of the potentiometer 58 provides the voltage excitation for the potentiometer 52.
  • any error in range is compensated for by setting switch S6 to position (b).
  • Knobs S10 and S11 are set to the known target grid coordinates used for the registration.
  • Knobs S12 and S14 are left at the positions finally determined by the registration.
  • Switch S1 is set to position (b) and the input to voltmeter 56 is nulled by adjusting potentiometer 58 with knob S8. This will provide the same percentage adjustment for all subsequent settings of potentiometer 52 and the reading from knob S14 of the range from the weapon to the target will be that used to fire the weapon because the correction has been automatically introduced by the circuitry.
  • Another adjustment which may have to be made is the adjustment based on the difference in altitude between the weapon and the target. If the altitude of the target is either higher or lower than the altitude of the weapon, the weapon must be fired at an apparent range which is different from the actual geometric range from the weapon to the target. For example, if the target is at an altitude higher than the weapon, the weapon must be fired at an apparent range which is greater than the actual geometric range to be able to hit the target. When the weapon is an 81 mm mortar the change in the range used to account for the difference in altitude is equal to one-half of the difference between the altitude of the weapon and the altitude of the target.
  • a potentiometer 66 is provided.
  • the potentiometer 66 is operated by knob S9.
  • a two-position switch 68 provides either positive or negative voltage to the potentiometer 66 depending upon whether the altitude of the target is higher or lower than the altitude of the weapon.
  • the knob S9 is turned to a position representing the difference in altitude.
  • Switch 68 is then turned to either positive or negative.
  • the voltage excitation to potentiometer 66 is scaled so that its voltage output represents one-half of the altitude difference set in.
  • This output is coupled to the summing junction 50 to be added to or subtracted from the range signal from the resolver 40. Then when knob S14 is rotated to null the output of summing junction 50, the dial coupled to knob S14 will give the apparent firing range and not the actual geometric range. This apparent range will reflect both the registration and the altitude corrections.
  • the fire control computer of the present invention may be used for many types of weapon firing.
  • the tire control computer may be used advantageously for the firing of mortars.
  • FIG. 3 shows an operators panel for a fire control computer used for mortar firing.
  • the switches, knobs and dials are identified with reference numbers which correspond to the reference numbers used in the circuit diagrams of FIGS. 2A and 2B.
  • Knob S1 in the upper lefthand corner of FIG. 3 operates all sets of contact for the switch 81. Further, when knob S1 is pushed, it operates the push-to-close power switch 12. The dial of the null detector 56 is displayed above the knob S1.
  • Knob S2 operates the resolver 30 which represents the direction angle from the observer to the target A mechanical counter 70 is geared directly to knob S2 to provide a visual reading of the direction angle in mils.
  • Knob S3 operates potentiometer 28 which represents the range from the observer to the target R A mechanical counter 72 is geared directly to the knob S3 to provide a visual reading of the range from the observer to the target in meters.
  • Knob S4 operates potentiometer 20 which represents the grid east coordinate of the observer.
  • Knob S4 is geared directly to a mechanical counter 74 which visually displays the grid east coordinate.
  • the output of potentiometer 20 is representative of the algebraic difference between the observer grid east coordinate and the weapon grid east coordinate.
  • One method of setting the potentiometer to the algebraic difference between the two coordinates while having the counter 74 read directly in the observer grid east coordinate is to have the knob S4 connected to the potentiometer 20 through a spring loaded mechanical clutch mechanism. By pulling out the knob against the spring pressure, the clutch is disengaged. The operating procedure would be that the potentiometer 20 would first be set to electrical zero. Then the clutch is disengaged and the mechanical counter 74 is set to the weapon grid coordinate. Next, the clutch is engaged and the counter 74 is set to the observer grid coordinate. The net effect is that the mechanical counter 74 reads in the observer grid coordinates directly while the output of the potentiometer 20 represents the algebraic difference between the observer grid east coordinate and the weapon grid east coordinate.
  • Knob S5 operates potentiometer 22 which represents the observer grid north coordinate. Knob S5 will be geared directly to a mechanical counter 76 to provide visual indication of the observer grid north coordinate. Knob S5 will be identical in operation to knob S4. Knob S6 operates switch 86 which selects either the observer input information in position (a) or the target coordinate information in position (b).
  • Knob S7 operates potentiometer 62 which represents the registration point adjustment for the direction angle from the weapon to the target.
  • Knob S8 operates potentiometer 58 which represents the registration point adjustment for the range from the weapon to the target.
  • Knob 89 operates potentiometer 66 and is coupled to mechanical counter 78 to give a visual reading of the altitude correction in meters.
  • Two-position switch 68 provides the proper polarity for the altitude correction.
  • Knob S10 operates potentiometer 24 and is geared to mechanical counter 80 to provide a representation of the target grid east coordinate.
  • Knob S11 operates potentiometer 26 and is coupled to mechanical counter 82 to provide a representation of the target grid north coordinate.
  • Knobs S10 and S11 operate in a manner identical to knob S4 with the clutch mechanism to provide the difference between the target coordinates and the weapon coordinates.
  • Knob S12 operates resolver 40 and is coupled to mechanical counter 84 to provide a representation of the direction from the weapon, in this case a mortar, to the target.
  • Knob S14 operates potentiometer 52 and is coupled to mechanical counter 86 to provide a representation of the range from the weapon, in this case the mortar, to the target.
  • the function of knobs S15 and S16 will be explained later.
  • the information required for firing of a weapon is the direction angle from the grid north coordinate and the elevation of the weapon and the charge to be used in firing the weapon.
  • the elevation and charge are functions of the range from the weapon to the target.
  • the weapon firing personnel consult a chart for the particular ammunition being used which gives values for the elevation and charge which correspond to the particular range. There is usually some overlap in the chart for various levels of charge. For example, for a particular range, a certain charge and elevation may be provided by the table. Also, for the same range, a greater charge and a greater elevation may be provided. This gives some flexibility to the weapon firing personnel to control the trajectory of the ammunition. In any case, once the range from the weapon to the target has been determined, the remaining firing information may be obtained.
  • the firing Table 13 is shown as a plug-in cassette.
  • the plug-in cassette may be geared directly to the range knob S14. In this way, when the range is set on knob S14, the weapon firing personnel may read the elevation and charge directly from the firing table cassette. By sliding the cover to either the right or the left, two sets of elevation and charge can be read for the input range setting.
  • the firing table cassette while being a convenience to the weapon firing personnel, is not critical for the operation of the present invention.
  • the weapon firing personnel may read the range figure from the mechanical counter 86 and then look up the appropriate elevation and charge from a firing table which may be separate from weapon firing computer.
  • the weapon firing computer described in FIGS. 2A, 2B and 3 will provide all necessary weapon firing information for the firing of an 81 millimeter mortar.
  • the 81 millimeter mortar has a continuously variable elevation and uses ammunition with up to nine increments of charge variation.
  • the weapon firing computer may accommodate a 4.2 inch mortar.
  • the 4.2 inch mortar differs somewhat from the 81 millimeter mortar in that the 4.2 inch mortar is normally fired from one of three fixed elevation angles.
  • a round of ammunition comes with or without extension.
  • the extension is a tubular piece added on the rear of the ammunition round, containing additional charges. Range is adjusted by changing the amount of propelling charge, in one-eighth charge increments.
  • FIG. 2C shows the same circuitry as shown in FIG. 2B with the additional circuitry necessary to accommodate the 4.2 inch mortar.
  • a selector switch S16 is provided with an off position that disconnects the circuitry for the 4.2 inch mortar.
  • the selector switch S16 also has six additional positions to select one of the three elevation angles with or without ammunition extension.
  • the range from the weapon to the target R is determined following the procedures previously described.
  • the range R will be set on knob S14.
  • the range must be converted to the amount of charge required. This is accomplished by providing a potentiometer 90 which is also set by knob S14.
  • Potentiometer 90 represents the relationship between charge and range which is a linear function. However, the slope of the linear relationship is different for each of the ammunition/elevation choices.
  • a set of six resistors 92 is used to change the scale factor for potentiometer 90 in accordance with the setting of selector switch S16.
  • the output of potentiometer 90 is coupled to one input of a summing junction 94.
  • the altitude correction is set on potentiometer 66 by knob S9 as previously described.
  • the only alteration required for the 4.2 inch mortar is to adjust the scale factor for the ammunition/elevation choices.
  • a set of six resistors 96 is used to change the scale factor for potentiometer 66 in accordance with the setting of selector switch S16.
  • the output of potentiometer 66 is switched to a second input to summing junction 94 when selector switch S16'is in any position except OFF.
  • the output of summing junction 94 is representative of the charge required for the range set on knob S14 for the particular ammunition/elevation combination selected. In order to provide a charge readout, the output of summing junction 94 is coupled to one input of a summing junction 98.
  • a potentiometer 100 is provided to represent the total charge required. Potentiometer 100 is operated by handset knob S15 and its output is coupled to a second input of summingjunction 98. The output of summing junction 98 is coupled to contact (c) of switch S1.
  • knob S15 is rotated until a null is reached on meter 56. The rotation of knob S15 is then representative of the total charge. Knob S15 may be coupled to a mechanical counter 102 shown in FIG. 3 to provide a visual readout of the charge.
  • the 4.2 inch mortar round is spin stabilized and will drift in flight due to the spin. This requires a direction angle correction as a function of range.
  • the amount of the drift correction is a nonlinear function of range. However, the relationship may be approximated by two linear functions.
  • the drift correction starts at some fairly high value for short range distances. The correction decreases as range increases up to some point after which the correction increases as range increases.
  • the direction angle drift correction is provided by a potentiometer 104 which is operated by knob S14.
  • the potentiometer 104 has three voltage inputs which are scaled by sets of resistors 106, 108 and 110 for the possible elevations. The lowest voltage is applied to a point along the potentiometer winding representative of the point on the drift correction vs. range curve where the slope of the curve changes from negative to positive.
  • the output of potentiometer 104 is coupled to a summing junction 112.
  • the direction adjustment for potentiometer 62 is coupled to a second input of summing junction 112.
  • the output of summing junction 112 is then representative of the total direction angle correction and is coupled to divider 64.
  • the weapon firing computer may be operated by relatively non-skilled operators simply by turning knobs and switches following a fixed step by step procedure. In practice a procedure chart would be provided to minimize the chance for operator error.
  • circuitry for mortar firing has been described, it should be apparent that the circuitry may be modified to account for the special requirements of other types of weapon firing such as artillery.
  • a weapon site gunner operated computer for determining the range and direction angle from a weapon positioned at known grid coordinates to a target, said computer comprising:
  • handset data means for converting gunner handset data into computer instrumented representations thereof
  • first circuit means responsive to a first portion of said representations of said handset data which are a measure of known factors in the trigonometric relation between an observers position, the target position, and the weapon position for providing signals representative of the target grid coordinates in relation to the weapon grid coordinates;
  • second circuit means responsive to a second portion of said representations of said handset data which are a measure of unknown factors in said trigonometric relation and to the signals of said first circuit means, for providing a null balance signal when said second portion of said representations comprises a correct representation of the range from the weapon to the target and the direction angle from the weapon to the target.
  • said first circuit means includes means for converting the range and direction angle from an observer at known grid coordinates relative to the weapon, to signals representative of the target grid coordinates in relation to the weapon grid coordinates.
  • said second circuit means includes a circuit coupled to receive the signals of said first circuit means for providing a first signal representative of the direction angle from the weapon to the target and a second signal representative of the range from the weapon to the target,
  • a computer as claimed in claim 3 which further comprises:
  • said first circuit means comprises:
  • a first potentiometer having its shaft position provided by said handset data means for providing an analog signal representative of the range from an observer position to the target;
  • a first resolver having the angular position of its shaft provided by said handset data means, the angular position of the resolver shaft being representative of the direction angle from the observer to the tarsaid first resolver being coupled to receive the analog signal of said first potentiometer for providing a first signal representative of the range from the observer position to the target times the cosine of the direction angle from the observer to the target, and a second signal representative of the range from the observer position to the target times the sine of the direction angle from the observer to the target;
  • a second potentiometer having its shaft position provided by said handset data means for providing an analog signal representative of the difference between the observer grid north coordinate and the weapon grid north coordinate;
  • a third potentiometer having its shaft position provided by said handset data means for providing an analog signal representative of the difference between the observer grid east coordinate and the weapon grid east coordinate;
  • a first summing means coupled to receive the first signal of said resolver and the analog signal of said second potentiometer for providing an output signal representative of the difference between the target grid north coordinate and the weapon grid north coordinate;
  • a second summing means coupled to receive the second signal of said resolver and the analog signal of said third potentiometer for providing an output signal representative of the difference between the target grid east coordinate and the weapon grid east coordinate;
  • a fourth potentiometer having its shaft position provided by said handset data means for providing an analog signal representative of the difference between the target grid north coordinate and the weapon grid north coordinate;
  • a fifth potentiometer having shaft position provided by said handset data means for providing an analog signal representative of the difference between the target grid east coordinate and the weapon grid east coordinate;
  • manual switching means coupled to provide a first output and a second output, said first output being the output signal of said first summing means when said manual switching means is in a first position and said first output being the analog signal of said fourth potentiometer when said manual switching means is in a second position; said second output being the output signal of said second summing means when said manual switching means is in a first position and said second output being the analog signal of said fifth potentiometer when said manual switching means is in a second position.
  • a computer as claimed in claim 5 wherein said second circuit means comprises:
  • a second resolver having the angular position of its shaft provided by said handset data means, and being coupled to receive the first and second outputs of said manual switching means for providing a first signal equal to zero when the angular position of the shaft of said second resolver represents the direction angle from the weapon to the target, and a second signal representative of the range from the weapon to the target;
  • signal detecting means coupled to receive the first signal of said second resolver for detecting when the signal is essentially equal to zero.
  • a computer as claimed in claim 6 which further comprises:
  • a sixth potentiometer having its shaft position provided by said handset data means for providing an analog signal representative of the range from the weapon position to the target;
  • a third summing means coupled to receive the analog signal of said sixth potentiometer and the second signal of said second resolver for providing an output signal which is the difference between the two input signals;
  • signal detecting means coupled to receive the output signal of said third summing means for detecting when the signal is essentially equal to zero.
  • a gunner operated weapon firing computer for determining the range and direction angle from a weapon positioned at known grid coordinates to a target, said weapon firing computer comprising:
  • handset data means for converting gunner handset data into shaft position
  • a first potentiometer having its shaft position provided by said handset data means for providing an analog signal representative of the range from an observer position to the target;
  • a first resolver having the angular position of its shaft provided by said handset data means, the angular position of the resolver shaft being representative of the direction angle from the observer to the tarsaid first resolver being coupled to receive the analog signal of said first potentiometer for providing a first signal representative of the range from the observer position to the target times the cosine of the direction angle from the observer to the target, and a second signal representative of the range from the observer position to the target times the sine of the direction angle from the observer to the target;
  • a second potentiometer having its shaft position provided by said handset data means for providing an analog signal representative of the difference between the observer grid north coordinate and the weapon grid north coordinate;
  • third potentiometer having its shaft position provided by said handset data means for providing an analog signal representative of the difference between the observer grid east coordinate and the weapon grid east coordinate;
  • first summing junction coupled to receive the first signal of said resolver and the analog signal of said second potentiometer for providing an output signal representative of the difference between the target grid north coordinate and the weapon grid north coordinate;
  • second summing junction coupled to receive the second signal of said resolver and the analog signal of said third potentiometer for providing an output signal representative of the difference between the target grid east coordinate and the weapon grid east coordinate;
  • manual switching means coupled to provide a first the output signal of said first summing junction when said manual switching means is in a first position and said first output being the analog signal of said fourth potentiometer when said manual switching means is in a second position; said second output being the output signal of said second summing junction when said manual switching means is in a first position and said second output being the analog signal of said fifth potentiometer when said manual switching means is in a second position;
  • second resolver having the angular position of its shaft provided by said handset data means and coupled to receive the first and second outputs of said manual switching means for providing a first signal equal to zero when the angular position of the resolver shaft represents the direction angle from the weapon to the target, and a second signal representative of the range from the weapon to the target;
  • signal detecting means coupled to receive the first signal of said second resolver for detecting when the signal is essentially equal to zero.
  • a weapon firing computer as claimed in claim 8 which further comprises:
  • a sixth potentiometer having its shaft position provided by said handset data means for providing an analog signal representative of the range from the weapon position to the target;
  • a third summing junction coupled to receive the anasignal detecting means coupled to receive the output signal of said third summing junction for detecting when the signal is essentially equal to zero.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Computer Hardware Design (AREA)
  • Physics & Mathematics (AREA)
  • Theoretical Computer Science (AREA)
  • Mathematical Physics (AREA)
  • General Physics & Mathematics (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
US00171055A 1971-08-12 1971-08-12 Weapon firing computer Expired - Lifetime US3739153A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US17105571A 1971-08-12 1971-08-12

Publications (1)

Publication Number Publication Date
US3739153A true US3739153A (en) 1973-06-12

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ID=22622312

Family Applications (1)

Application Number Title Priority Date Filing Date
US00171055A Expired - Lifetime US3739153A (en) 1971-08-12 1971-08-12 Weapon firing computer

Country Status (9)

Country Link
US (1) US3739153A (OSRAM)
JP (1) JPS4835742A (OSRAM)
BE (1) BE787434A (OSRAM)
CA (1) CA967282A (OSRAM)
DE (1) DE2238218A1 (OSRAM)
FR (1) FR2150086A5 (OSRAM)
GB (1) GB1389587A (OSRAM)
IT (1) IT961947B (OSRAM)
NL (1) NL7211061A (OSRAM)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4146780A (en) * 1976-12-17 1979-03-27 Ares, Inc. Antiaircraft weapons system fire control apparatus
EP0016490A1 (de) * 1979-03-23 1980-10-01 Werkzeugmaschinenfabrik Oerlikon-Bührle AG Verfahren zum indirekten Richten eines Geschützes und Einrichtung zur Durchführung des Verfahrens
US20040024566A1 (en) * 2002-07-31 2004-02-05 Chris Hogan Mortar ballistic computer and system
RU2226715C2 (ru) * 1987-04-27 2004-04-10 Московский государственный институт электронной техники (технический университет) Танковый баллистический вычислитель

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2459443A1 (fr) * 1979-06-15 1981-01-09 Thomson Brandt Procede et dispositif de determination des elements de tir d'un projectile
US5481957A (en) * 1992-07-06 1996-01-09 Alliedsignal Inc. Aiming and pointing system for ground based weapons equipment

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4146780A (en) * 1976-12-17 1979-03-27 Ares, Inc. Antiaircraft weapons system fire control apparatus
EP0016490A1 (de) * 1979-03-23 1980-10-01 Werkzeugmaschinenfabrik Oerlikon-Bührle AG Verfahren zum indirekten Richten eines Geschützes und Einrichtung zur Durchführung des Verfahrens
US4409468A (en) * 1979-03-23 1983-10-11 Werkzeugmaschinenfabrik Oerlikon-Buhrle Ag Method for indirectly laying a weapon and apparatus for the performance of the method
RU2226715C2 (ru) * 1987-04-27 2004-04-10 Московский государственный институт электронной техники (технический университет) Танковый баллистический вычислитель
US20040024566A1 (en) * 2002-07-31 2004-02-05 Chris Hogan Mortar ballistic computer and system
US7526403B2 (en) 2002-07-31 2009-04-28 Dahlgren, Llc Mortar ballistic computer and system

Also Published As

Publication number Publication date
CA967282A (en) 1975-05-06
JPS4835742A (OSRAM) 1973-05-26
IT961947B (it) 1973-12-10
DE2238218A1 (de) 1973-02-22
BE787434A (fr) 1972-12-01
GB1389587A (en) 1975-04-03
NL7211061A (OSRAM) 1973-02-14
FR2150086A5 (OSRAM) 1973-03-30

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