US2115086A - Nonhunting or dead beat remote control - Google Patents

Nonhunting or dead beat remote control Download PDF

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US2115086A
US2115086A US690693A US69069333A US2115086A US 2115086 A US2115086 A US 2115086A US 690693 A US690693 A US 690693A US 69069333 A US69069333 A US 69069333A US 2115086 A US2115086 A US 2115086A
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motor
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speed
generator
tubes
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Alger S Riggs
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Sperry Gyroscope Co Inc
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Sperry Gyroscope Co Inc
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    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D3/00Control of position or direction
    • G05D3/12Control of position or direction using feedback
    • G05D3/121Control of position or direction using feedback using synchromachines (selsyns)
    • G05D3/122Control of position or direction using feedback using synchromachines (selsyns) without modulation

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  • I combine 0 the signal voltage from the controller with a voltage generated as a function of the direction and speed of rotation of the motor with the result that for every position of the controller or relative position of the controller and controlled objects there is a definite motor speed so that if the controller approaches or reaches its zero position while the motor, due to the inertia of the armature or load, is still rotating at good speed there is impressed a counter E. M. F. on
  • the motor amounting to a reversal of the torque producing current thus bringing the motor quickly to rest by the time the controller has reached the zero position.
  • Fig. 1 is a wiring diagram showing how my invention may be applied to the control of the speed and direction of a power motor from a distance.
  • a power motor from a distance.
  • Such a system might be adapted for use for multiple unit electric train control or for the control of the speed of the driving motors of sound picture projectors, etc.
  • Fig. 2 is a similar wiring diagram showing my invention as applied to a system for reproducing the position of a controlling object by a receiving 5 object, such as between the pilot house and rudder of a ship or between a telescope or sound locator and a searchlight or as a follow-up system.
  • a receiving 5 object such as between the pilot house and rudder of a ship or between a telescope or sound locator and a searchlight or as a follow-up system.
  • the controller I in Fig. 1 is represented as a vario-coupled transformer in which the secondary 2 is rotatable with respect to the primary by means of a controller handle I so that the voltages induced therein may be varied from zero when the coils are at right angles to a maximum in one phase relationship or polarity or in the other, dependent on whether the controller is rotated clockwise or anti-clockwise.
  • the signals from the controller may be supplied to a transformer I by means of which opposite phases are applied to the grids 01 a pair of electron tubes 5 and 6 through suitable resistances I and 8 in such a manner that the phases on the grids of the two tubes are oppositely shifted in accordance with the magnitude and direction of the signal.
  • a transformer I by means of which opposite phases are applied to the grids 01 a pair of electron tubes 5 and 6 through suitable resistances I and 8 in such a manner that the phases on the grids of the two tubes are oppositely shifted in accordance with the magnitude and direction of the signal.
  • I have shown a system of dynamic phase shift described and claimed in the prior patent of Francis L. Moseley, No. 2,088,859, dated August 3, 1937, for Phase shift control of electron tubes, in which a bias voltage is added to the signal voltage to produce a phase shift on the grid.
  • a phase shift net work employing a transformer 9, having a center tap leading to a center tap on the transformer 4, is employed, the primary being excited directly from the supply and a bias voltage being produced by any suitable means, such as a condenser l0 and a resistance Ii connected in circuit to the cathodes of the tubes.
  • the heater winding of all tubes is omitted for sake of-clearness.
  • the output of the two tubes is led through suitable transformers I2 and i3 which control the speed and direction of the power motor I4.
  • a very simple form of power motor adapted for use in this circuit is a reversible repulsion motor, the field of which is continuously excited from the supply and the two pair of brushes respectively short circuited through the secondaries of the transformers l2 and II.
  • the tubes act as variable resistances shunted across the brushes as explained more fully in the copending application of said Francis L. Moseley, now Patent #2,008,364, dated July 16, 1935, for Remote control of heavy objects.
  • the motor armature is shown as coupled to a load I5 through gearing l6.
  • the rotor may comprise merely a thin copper cylinder 2
  • the induced voltages in coil 20 may be coupled directly in circuit between signal 2 and the primary 4' of transformer 4 so as to superimpose this voltage on the signal voltage with the result that the signal actually impressed on the transformer I is the resultant of the external signal and the voltage generated as a function of the direction and speed of the motor.
  • phase correctors 24 and 24 With my system, therefore, the motor ll will have a definite speed for each position of the controller since, as the controller is moved from point to point, the strength of the signal will rise until the speed of the motor is such as to impress a counter signal which will hold the resultant signal to the fixed value.
  • FIG. 2 the sending device is shown as a pilot wheel 3 of a ship, to which is coupled a suitable inductive device I which is of a type often used for transmitting angular motion and is shown as comprising a field 25 excited from a single phase supply and an armature having a multi-tapped winding connected to a similar winding 26' on a similar inductive device driven by the receiver or the motor I4 turning the same.
  • a suitable inductive device I which is of a type often used for transmitting angular motion and is shown as comprising a field 25 excited from a single phase supply and an armature having a multi-tapped winding connected to a similar winding 26' on a similar inductive device driven by the receiver or the motor I4 turning the same.
  • the generator H in this case, is shown as driven by step-up gearing ill from the shaft 28 of the power motor l4. Said shaft is also shown as driving the armature 26' through gearing 32 and shaft 33. In this instance the generator is shown as an ordinary commutator type, single phase generator in which the field I9 is excited from the supply. The armature, therefore, will generate an A. C. voltage of the same frequency as the supply and which varies in magnitude and polarity with the direction and speed of the motor. Said armature is shown as coupled between the signal supplied by the coil 21 and the input transformer 29.
  • a somewhat different form of tube control is also shown in this figure.
  • the grid circuits of the two tubes 5' and 6' are connected in parallel to the transformer 29, while the plates of said tubes are connected in opposition or push-pull fashion to transformers l2 and I3.
  • a source of direct current may be inserted to bias the tubes to prevent starting until the grid swings to a predetermined potential.
  • the tubes are either full on or entirely 03, giving a sensitive control which would be unstauie without my hunt preventing and speed control generator previously described but which is remarkably dead beat and accurate when my invention is applied thereto.
  • the rudder or other controlled object may be accurately and quickly positioned in accordance with the movements of the controller without overshooting.
  • the pilot desires to turn sharply. He rotates the pilot wheel quickly to swing the rudder 35 through the desired angle. This results in a large signal being sent to the tubes resulting in a quick pick-up of the motor. As the motor speeds up, however, a point will be reached where the voltage generated by the generator I! will prevent further increase in speed.
  • the armature 26' of the receiver is turned with the rudder and motor l4 so that the signal voltage becomes weaker and weaker until it becomes zero.
  • Means for reproducing position at a distance comprising an A. C. power motor, an A. C. power source therefor, a signal sending device also powered from said source, an A. C. generator driven by said motor, the output of which is normally in phase opposition to the signal of said sending, device, means including electron discharge tubes for controlling the speed and direction of said motor in accordance with signal voltages impressed on said tubes, said signal voltages comprising the resultant of the external signal from said device, and a voltage generated by said generator as a function of the direction and speed of rotation of said motor.
  • a remote positional control for heavy objects the combination with a reversible motor and alternating current source, of sending and receiving inductive devices for supplying voltages varying in direction and magnitude in accordance with the relative position of the sending and receiving devices, the latter being positioned by said motor and the motor being governed by the output of said devices, an additional generator driven by said motor, and means for impressing the output thereof on the input circuit to the motor.
  • Means for rotating an object to maintain it in positional agreement with a remote controlling object comprising an A. C. electric power motor for rotating the driven object, a weak alternating current signal means, the output of which is dependent in amount and phase on the relative position of said objects, electron tube means controlled by said A. C. signal to cause actuation of said motor to drive the driven object, and electric means responsive to the speed and direction of said motor for generating an A. C. electromotive force counter to that supplied by said signal to said tube means and also supplied to the latter for preventing overrunning of said motor.
  • Means for reproducing position comprising, in combination with a controlling and a driven object, means for producing an A. C. signal which varies in magnitude and direction with the amount and direction of variation in position between said objects, an A. C. generator driven by said driven object and producing an A. C. signal oi like frequency with said other signal and which varies in magnitude and direction with the speed and direction of rotation of the driven object, an electron tube circuit governed by said combined signals, and a motor controlled by the output of said circuit for driving the driven object.
  • Means for reproducing position comprising in combination with a controlling object and a driven object, a field winding and a poly-circuit armature winding relatively rotated by said controlling object in a predetermined angular relation therewith, a source of alternating current supply connected to said field winding, a second poly-circuit armature winding electrically connected to said first armature winding so as to produce an alternating magnetic field moving with said controlling object, a motor for driving said driven object, a coil in said field, one oi.
  • said coil and second windings being driven by said motor, means responsive to the electromotive force induced in said coil for controlling said motor so as to cause the motor to drive the driven object into positional agreement with the controlling object, and an alternating current generator driven by said motor, the electromotive force generated by which is proportional to its velocity, said electromotive force being superimposed on the electromotive force supplied by said coil to control said motor, whereby overrunning is prevented.
  • Means for reproducing position comprising, in combination with a controlling and a driven object and an A. C. source, means for producing an A. C. signal which varies in magnitude and direction with the amount and direction of variation in position between said objects, a rotor having an outer ring oi! non-magnetic but electrically conductive material and an inner iron core supporting said ring and rotated bysaid driven object, two field windings adjacent said rotor arranged in quadrature, one of said windings being excited from said A. C. source, and a motor for driving said driven element controlled by the combined output of said signal and said second winding on said rotor.
  • a remote positional control for rotatable objects the combination with an A. C. sending device, an A. C. reversible motor for turning said object with said device, an alternating current source, means for governing the speed and direction of said motor including an electron tube also powered from said source, said sending device furnishing a controlling signal of variable magnitude and direction governed by the relative positions of said device and object for governing the speed and direction of said motor, a rotor having a cylindrical member of non-magnetic electrical conducting material mounted on an iron core rotated by said motor, a field winding supplied from said A. C. source and positioned so that its field is intersected bysaid member, and a. second field winding arranged in quadrature to said first field winding and electrically connected to oppose the input signal to said tube.
  • a remote positional control for rotatable objects the combination with a sending device, a reversible motor for turning said object with said device, an alternating current source for energizing said sending device and for supplying said motor, means for governing the speed and direction of said motor including an electron tube also powered from said source, said sending device serving to supply a controlling signal of variable magnitude and direction governed by the relative positions of said device and object for governing the speed and direction of said motor, a rotor having a hollow cylindrical member of non-magnetic electrical conducting material provided with an iron core and rotated from said motor, a field winding supplied from said source and arranged so that its field extends transversely through said cylindrical member, and a winding arranged at right angles to said field winding and connected to oppose the input signal to said tube.
  • a remote positional control the combination with an alternating current source, 9. sending device of limited power energized by said source, a remote controlled device requiring power motor actuation, a reversible power motor for turning said controlled device, means including an electron tube supplied from said sending device with a controlling signal of varying magnitude and direction for governing the speed and direction oi. said motor in accordance with the magnitude and direction of variance between the sending and controlled devices, a small alternating current generator driven by said motor having its field excited from said source, and means for impressing the output thereof in opposition to the input signal to said tube.

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  • General Physics & Mathematics (AREA)
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  • Control Of Direct Current Motors (AREA)

Description

April 26, 1938. A. s. RIGGS 2,115,086
NONHUNTING OR DEAD BEAT REMOTE CONTROL Filed Sept. 23, 1933 Mg g i LOAD ql'gd.
5 INVENT R H15 ATTOFQNEY.
Patented Apr. 26, 1938 UNITED STATES PATENT OFFICE NONHUN TING OB DEAD BEAT REMOTE CONTRO Application September 23, 1933, Serial No. 890,693 9 Claims. (01. 172-239) This invention relates to improvements in the remote control of movable objects and more especially to means for controlling electric motors of considerable power and driving loads of considerable inertia from a low power controller. In most systems of this type, there is a marked tendency to hunt or overshoot the position of rest so that the system becomes oscillatory and unstable. According to my invention, I combine 0 the signal voltage from the controller with a voltage generated as a function of the direction and speed of rotation of the motor with the result that for every position of the controller or relative position of the controller and controlled objects there is a definite motor speed so that if the controller approaches or reaches its zero position while the motor, due to the inertia of the armature or load, is still rotating at good speed there is impressed a counter E. M. F. on
the motor amounting to a reversal of the torque producing current thus bringing the motor quickly to rest by the time the controller has reached the zero position.
Referring to the drawing,
Fig. 1 is a wiring diagram showing how my invention may be applied to the control of the speed and direction of a power motor from a distance. Such a system might be adapted for use for multiple unit electric train control or for the control of the speed of the driving motors of sound picture projectors, etc.
Fig. 2 is a similar wiring diagram showing my invention as applied to a system for reproducing the position of a controlling object by a receiving 5 object, such as between the pilot house and rudder of a ship or between a telescope or sound locator and a searchlight or as a follow-up system. i
In both figures the source of power is-shown as single phase alternating current, although obviously my invention is not limited thereto. The controller I in Fig. 1 is represented as a vario-coupled transformer in which the secondary 2 is rotatable with respect to the primary by means of a controller handle I so that the voltages induced therein may be varied from zero when the coils are at right angles to a maximum in one phase relationship or polarity or in the other, dependent on whether the controller is rotated clockwise or anti-clockwise. The signals from the controller may be supplied to a transformer I by means of which opposite phases are applied to the grids 01 a pair of electron tubes 5 and 6 through suitable resistances I and 8 in such a manner that the phases on the grids of the two tubes are oppositely shifted in accordance with the magnitude and direction of the signal. For this purpose I have shown a system of dynamic phase shift described and claimed in the prior patent of Francis L. Moseley, No. 2,088,859, dated August 3, 1937, for Phase shift control of electron tubes, in which a bias voltage is added to the signal voltage to produce a phase shift on the grid. For this purpose a phase shift net work employing a transformer 9, having a center tap leading to a center tap on the transformer 4, is employed, the primary being excited directly from the supply and a bias voltage being produced by any suitable means, such as a condenser l0 and a resistance Ii connected in circuit to the cathodes of the tubes. The heater winding of all tubes is omitted for sake of-clearness. The output of the two tubes is led through suitable transformers I2 and i3 which control the speed and direction of the power motor I4. A very simple form of power motor adapted for use in this circuit is a reversible repulsion motor, the field of which is continuously excited from the supply and the two pair of brushes respectively short circuited through the secondaries of the transformers l2 and II. In such a circuit the tubes act as variable resistances shunted across the brushes as explained more fully in the copending application of said Francis L. Moseley, now Patent #2,008,364, dated July 16, 1935, for Remote control of heavy objects. The motor armature is shown as coupled to a load I5 through gearing l6.
While the system so far described would turn the motor on and of! with a limited speed control, it has no accurate speed control and would overshoot the position of rest, and if employed in a follow-up system would continually hunt, and it is to the securing of accurate speed control and the preventing of hunting that this invention is mainly directed. For this purpose I couple to the motor ll, or what amounts to the same thing, to the load IS, a generator I! through suitable gearing I8. Said generator is so designed as to produce an alternating current electromotive force normally in opposition to or out of phase with the signal supplied from the controller 2 ,in Fig. 1 or 21 in Fig. 2, which electromotive force varies in direction and magnitude with the direction and speed of the motor or load. To accomplish this special function in the best manner requires a special type of generator which I have shown in Fig. 1 and term a field distorting generator or dynamic transformer.
It is shown as having two fields II and 2|, the former excited from the line and the latter placed at right angles thereto. The rotor may comprise merely a thin copper cylinder 2| on an iron core 22. When the armature is stationary, no voltage is induced in the field but as the armature is rotated the lines of force from the field l9 are distorted to pass through a coil 20, the amount of the distortion varying from zero at zero speed and approaching 90' at high speeds. The induced voltages in coil 20 may be coupled directly in circuit between signal 2 and the primary 4' of transformer 4 so as to superimpose this voltage on the signal voltage with the result that the signal actually impressed on the transformer I is the resultant of the external signal and the voltage generated as a function of the direction and speed of the motor. It will be understood that the proper phase relationship is maintained in the system by means of suitable phase correctors 24 and 24. With my system, therefore, the motor ll will have a definite speed for each position of the controller since, as the controller is moved from point to point, the strength of the signal will rise until the speed of the motor is such as to impress a counter signal which will hold the resultant signal to the fixed value. v
A very important application of my invention is in the positional control of heavy objects from a distance, such as searchlights, guns or ships rudders. In Fig. 2 the sending device is shown as a pilot wheel 3 of a ship, to which is coupled a suitable inductive device I which is of a type often used for transmitting angular motion and is shown as comprising a field 25 excited from a single phase supply and an armature having a multi-tapped winding connected to a similar winding 26' on a similar inductive device driven by the receiver or the motor I4 turning the same. It will readily be seen, therefore, that no electro-motive force will be produced in a field 21 of the receiving device as long as the armatures I and 26 are in the same angular position, but that an alternating E. M. F. will be produced in the field 21 of a magnitude and direction or polarity, dependent on the relative turning of the sending and receiving instruments in one direction or the other. The. signal produced in 21, therefore, is quite similar to the signal produced in the winding 2 in Fig. 1. Said signal is also preferably combined with a counter signal generated by the rotation of the motor as in Fig. l.
The generator H, in this case, is shown as driven by step-up gearing ill from the shaft 28 of the power motor l4. Said shaft is also shown as driving the armature 26' through gearing 32 and shaft 33. In this instance the generator is shown as an ordinary commutator type, single phase generator in which the field I9 is excited from the supply. The armature, therefore, will generate an A. C. voltage of the same frequency as the supply and which varies in magnitude and polarity with the direction and speed of the motor. Said armature is shown as coupled between the signal supplied by the coil 21 and the input transformer 29.
A somewhat different form of tube control is also shown in this figure. In this instance the grid circuits of the two tubes 5' and 6' are connected in parallel to the transformer 29, while the plates of said tubes are connected in opposition or push-pull fashion to transformers l2 and I3. In addition, a source of direct current may be inserted to bias the tubes to prevent starting until the grid swings to a predetermined potential. In this system the tubes are either full on or entirely 03, giving a sensitive control which would be unstauie without my hunt preventing and speed control generator previously described but which is remarkably dead beat and accurate when my invention is applied thereto.
By my invention the rudder or other controlled object may be accurately and quickly positioned in accordance with the movements of the controller without overshooting. Suppose, for instance, that the pilot desires to turn sharply. He rotates the pilot wheel quickly to swing the rudder 35 through the desired angle. This results in a large signal being sent to the tubes resulting in a quick pick-up of the motor. As the motor speeds up, however, a point will be reached where the voltage generated by the generator I! will prevent further increase in speed. As the rudder approaches the desired position, the armature 26' of the receiver is turned with the rudder and motor l4 so that the signal voltage becomes weaker and weaker until it becomes zero. At the same time the counter voltage supplied by the generator II will be maintained as long as the motor speed persists so that if the inertia of the motor armature or rudder gives it a greater speed than the normal speed for any given relative position of the pilot wheel and rudder, a counter E. M. F. will be applied to quickly slow down the motor to the proper speed and bring it to rest by the time the rudder has reached the desired position.
In accordance with the provisions of the patent statutes, I have herein described the principle and operation of my invention, together with the apparatus which I now consider to represent the best embodiment thereof, but I desire to have it understood that the apparatus shown is only illustrative and that the invention can be carried out by other means. Also, while it is designed to use the various features and elements in the combination and relations described, some of these may be altered and others omitted without interfering with the more general results outlined, and the invention extends to such use.
Having described my invention, what I claim and desire to secure by Letters Patent is:
1. Means for reproducing position at a distance comprising an A. C. power motor, an A. C. power source therefor, a signal sending device also powered from said source, an A. C. generator driven by said motor, the output of which is normally in phase opposition to the signal of said sending, device, means including electron discharge tubes for controlling the speed and direction of said motor in accordance with signal voltages impressed on said tubes, said signal voltages comprising the resultant of the external signal from said device, and a voltage generated by said generator as a function of the direction and speed of rotation of said motor.
2. In a remote positional control for heavy objects the combination with a reversible motor and alternating current source, of sending and receiving inductive devices for supplying voltages varying in direction and magnitude in accordance with the relative position of the sending and receiving devices, the latter being positioned by said motor and the motor being governed by the output of said devices, an additional generator driven by said motor, and means for impressing the output thereof on the input circuit to the motor.
3. Means for rotating an object to maintain it in positional agreement with a remote controlling object, comprising an A. C. electric power motor for rotating the driven object, a weak alternating current signal means, the output of which is dependent in amount and phase on the relative position of said objects, electron tube means controlled by said A. C. signal to cause actuation of said motor to drive the driven object, and electric means responsive to the speed and direction of said motor for generating an A. C. electromotive force counter to that supplied by said signal to said tube means and also supplied to the latter for preventing overrunning of said motor.
4. Means for reproducing position comprising, in combination with a controlling and a driven object, means for producing an A. C. signal which varies in magnitude and direction with the amount and direction of variation in position between said objects, an A. C. generator driven by said driven object and producing an A. C. signal oi like frequency with said other signal and which varies in magnitude and direction with the speed and direction of rotation of the driven object, an electron tube circuit governed by said combined signals, and a motor controlled by the output of said circuit for driving the driven object.
5. Means for reproducing position comprising in combination with a controlling object and a driven object, a field winding and a poly-circuit armature winding relatively rotated by said controlling object in a predetermined angular relation therewith, a source of alternating current supply connected to said field winding, a second poly-circuit armature winding electrically connected to said first armature winding so as to produce an alternating magnetic field moving with said controlling object, a motor for driving said driven object, a coil in said field, one oi. said coil and second windings being driven by said motor, means responsive to the electromotive force induced in said coil for controlling said motor so as to cause the motor to drive the driven object into positional agreement with the controlling object, and an alternating current generator driven by said motor, the electromotive force generated by which is proportional to its velocity, said electromotive force being superimposed on the electromotive force supplied by said coil to control said motor, whereby overrunning is prevented.
6. Means for reproducing position comprising, in combination with a controlling and a driven object and an A. C. source, means for producing an A. C. signal which varies in magnitude and direction with the amount and direction of variation in position between said objects, a rotor having an outer ring oi! non-magnetic but electrically conductive material and an inner iron core supporting said ring and rotated bysaid driven object, two field windings adjacent said rotor arranged in quadrature, one of said windings being excited from said A. C. source, and a motor for driving said driven element controlled by the combined output of said signal and said second winding on said rotor.
7. In a remote positional control for rotatable objects, the combination with an A. C. sending device, an A. C. reversible motor for turning said object with said device, an alternating current source, means for governing the speed and direction of said motor including an electron tube also powered from said source, said sending device furnishing a controlling signal of variable magnitude and direction governed by the relative positions of said device and object for governing the speed and direction of said motor, a rotor having a cylindrical member of non-magnetic electrical conducting material mounted on an iron core rotated by said motor, a field winding supplied from said A. C. source and positioned so that its field is intersected bysaid member, and a. second field winding arranged in quadrature to said first field winding and electrically connected to oppose the input signal to said tube.
8. In a remote positional control for rotatable objects, the combination with a sending device, a reversible motor for turning said object with said device, an alternating current source for energizing said sending device and for supplying said motor, means for governing the speed and direction of said motor including an electron tube also powered from said source, said sending device serving to supply a controlling signal of variable magnitude and direction governed by the relative positions of said device and object for governing the speed and direction of said motor, a rotor having a hollow cylindrical member of non-magnetic electrical conducting material provided with an iron core and rotated from said motor, a field winding supplied from said source and arranged so that its field extends transversely through said cylindrical member, and a winding arranged at right angles to said field winding and connected to oppose the input signal to said tube.
9. In a remote positional control, the combination with an alternating current source, 9. sending device of limited power energized by said source, a remote controlled device requiring power motor actuation, a reversible power motor for turning said controlled device, means including an electron tube supplied from said sending device with a controlling signal of varying magnitude and direction for governing the speed and direction oi. said motor in accordance with the magnitude and direction of variance between the sending and controlled devices, a small alternating current generator driven by said motor having its field excited from said source, and means for impressing the output thereof in opposition to the input signal to said tube.
ALGER S. RIGGS.
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US2423337A (en) * 1942-05-25 1947-07-01 Sperry Gyroscope Co Inc Radio controlled pilot system
US2425317A (en) * 1943-07-13 1947-08-12 Sperry Gyroscope Co Inc Prediction apparatus
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US2464362A (en) * 1945-06-28 1949-03-15 Westinghouse Electric Corp Servomotor damper
US2471422A (en) * 1943-07-09 1949-05-31 Sperry Corp Position and speed control system
US2478279A (en) * 1945-07-07 1949-08-09 Curtiss Wright Corp Control system
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US2484089A (en) * 1946-12-31 1949-10-11 Rca Corp Motor speed control
US2489184A (en) * 1948-05-10 1949-11-22 Dynamatic Corp Electronic governing apparatus for electric machinery
US2488734A (en) * 1946-03-07 1949-11-22 Research Corp Dynamo transformer
US2492392A (en) * 1947-05-21 1949-12-27 Collins Radio Co Remotely tuned radio apparatus and the like
US2496809A (en) * 1941-02-10 1950-02-07 Sperry Corp Radio controlled pilot system
US2497216A (en) * 1945-09-28 1950-02-14 Rca Corp Servo system derivative generator
US2503346A (en) * 1943-10-01 1950-04-11 Smith & Sons Ltd S Automatic stabilizing control system
US2506798A (en) * 1943-08-06 1950-05-09 Barber Colman Co Stabilized power actuator and method of operating same
US2512665A (en) * 1943-10-18 1950-06-27 Smith & Sons Ltd S Electric motor control system
US2513537A (en) * 1945-07-20 1950-07-04 Williams Frederic Calland Electric integrator using a motor with velocity feedback
US2514555A (en) * 1941-06-21 1950-07-11 Bendix Aviat Corp Electric motor control system
US2526665A (en) * 1942-01-24 1950-10-24 Sperry Corp Positional control system
US2537027A (en) * 1947-02-08 1951-01-09 Duncan Electric Mfg Co Follow-up apparatus
US2538494A (en) * 1946-01-15 1951-01-16 Rca Corp Servo control amplifier
US2541666A (en) * 1945-05-12 1951-02-13 Curtiss Wright Corp Control system
US2545405A (en) * 1946-03-13 1951-03-13 Askania Regulator Co Electrical motor control system
US2548884A (en) * 1941-11-01 1951-04-17 Sperry Corp Remote positional control mechanism
US2567202A (en) * 1945-07-31 1951-09-11 Sperry Corp Eddy-current generator and control circuits
US2572986A (en) * 1945-03-22 1951-10-30 Chance Britton Radar tracking system
US2574104A (en) * 1946-07-01 1951-11-06 Ampro Corp Position and movement reproducing apparatus
US2582305A (en) * 1948-07-17 1952-01-15 Gen Electric Airplane maneuvering system
US2595868A (en) * 1947-05-05 1952-05-06 Smith & Sons Ltd S Automatic control system
US2604615A (en) * 1947-05-13 1952-07-22 Bendix Aviat Corp Engine speed control
US2605452A (en) * 1949-03-04 1952-07-29 Edward P Ney Stabilizing system using an amplidyne
US2620463A (en) * 1947-06-12 1952-12-02 Smith & Sons Ltd S Automatic control system
US2630282A (en) * 1948-09-10 1953-03-03 Sperry Corp Aircraft automatic pilot turn control system
US2642554A (en) * 1947-01-23 1953-06-16 Bendix Aviat Corp Automatic steering system
US2644642A (en) * 1953-07-07 Control system for a plurality of
US2646924A (en) * 1948-11-29 1953-07-28 Honeywell Regulator Co Computer for estimated time of arrival
US2650338A (en) * 1948-02-16 1953-08-25 Smith & Sons Ltd S Automatic aircraft control system
US2651014A (en) * 1949-03-24 1953-09-01 Honeywell Regulator Co Electronic amplifier with double frequency discriminator
US2664530A (en) * 1948-07-17 1953-12-29 Gen Electric Autopilot control system
US2686021A (en) * 1948-09-10 1954-08-10 Sperry Corp Aircraft automatic pilot turn control
US2689333A (en) * 1944-03-31 1954-09-14 Us Navy Magnetic stabilization system
US2694900A (en) * 1948-07-27 1954-11-23 Bendix Aviat Corp Aircraft engine power control to maintain selected combustion chamber temperature and engine speed conditions
US2695981A (en) * 1949-08-13 1954-11-30 Republic Flow Meters Co Follow-up type of measuring apparatus
US2700888A (en) * 1948-04-27 1955-02-01 Walter A Good Simulator for predicting the behavior of a roll-stabilized vehicle in flight
US2727201A (en) * 1952-07-29 1955-12-13 Gen Electric Motor control system
US2751535A (en) * 1953-06-18 1956-06-19 Alexander H Kuhnel Position control system
US2766413A (en) * 1954-02-10 1956-10-09 Allen E Young Position-sensitive probe circuit
US2769122A (en) * 1953-04-01 1956-10-30 Bendix Aviat Corp Self-balancing servo system
US2776397A (en) * 1954-03-04 1957-01-01 Bendix Aviat Corp Temperature compensated motor control system
US2783427A (en) * 1953-07-10 1957-02-26 W L Maxson Corp Motor control systems
US2795748A (en) * 1952-07-16 1957-06-11 Thompson Prod Inc Automatic speed control system using variable transmission
US2795747A (en) * 1952-07-16 1957-06-11 Thompson Prod Inc Automatic speed and stabilizing control using variable transmission
US2802160A (en) * 1954-11-09 1957-08-06 Gen Electric Intermediate zone locating servosystem
US2810103A (en) * 1954-12-13 1957-10-15 Cook Electric Co Multiple mode servomechanism
US2813236A (en) * 1949-01-14 1957-11-12 Sperry Rand Corp Control system for electric servomotors
US2825861A (en) * 1955-12-22 1958-03-04 Emerson Radio & Phonograph Cor Integrating servo mechanism
US2829323A (en) * 1955-07-29 1958-04-01 Digital Control Systems Inc Rate digital control system
US2832020A (en) * 1954-04-12 1958-04-22 Northrop Aircraft Inc Synchro system and quadrature voltage eliminator therefor
US2832028A (en) * 1953-10-09 1958-04-22 Sperry Gyroscope Co Ltd Positional control systems
US2843882A (en) * 1955-06-08 1958-07-22 Us Rubber Co Evener
US2847867A (en) * 1943-08-24 1958-08-19 Remco Electronic Inc Follow-up device
US2859397A (en) * 1955-12-28 1958-11-04 Gen Electric Feedback type control system
US2869059A (en) * 1954-12-13 1959-01-13 Cook Electric Co Follow-up control systems
US2875575A (en) * 1944-10-30 1959-03-03 Bendix Aviat Corp Control systems and apparatus for the power units of aircraft
US2881379A (en) * 1955-07-26 1959-04-07 Jr Benjamin F Logan Velocity servosystem with signal quadrature component suppression
US2885614A (en) * 1954-05-03 1959-05-05 United Aircraft Corp Servosystem angular motion transmitting apparatus
US2896142A (en) * 1956-12-12 1959-07-21 Bosch Arma Corp Servo controller
US2934689A (en) * 1957-11-22 1960-04-26 Gen Precision Inc Servo systems and quadrature signal filter therefor
US2939061A (en) * 1957-11-29 1960-05-31 American Machine & Metals Indicator servosystem
US2946942A (en) * 1955-07-01 1960-07-26 Amcel Propulsion Inc Thyratron control system
US2965828A (en) * 1958-07-24 1960-12-20 Gen Precision Inc Servo damping mechanism
US2996650A (en) * 1959-05-12 1961-08-15 Gen Precision Inc Servosystem with damping which decreases with servomotor speed
US3017556A (en) * 1957-03-18 1962-01-16 Republic Flow Meters Co Electrical servosystem control circuit
US3064173A (en) * 1956-05-18 1962-11-13 Celanese Corp Speed slaving method and apparatus
US3079539A (en) * 1960-08-15 1963-02-26 Fritz A Guerth Servosystem and pulse type amplifier
US3100277A (en) * 1958-09-08 1963-08-06 Stuart N Mccullough Switching servo system with anti-hunt feedback
US3100858A (en) * 1960-08-12 1963-08-13 Sperry Rand Corp Pressure rebalancing and measuring servosystem
US3108212A (en) * 1960-02-29 1963-10-22 Singer Inc H R B Duty-factor controlled motor
US3172025A (en) * 1960-05-16 1965-03-02 Gen Precision Inc Linear servo mechanism

Cited By (82)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2644642A (en) * 1953-07-07 Control system for a plurality of
US2420467A (en) * 1939-02-10 1947-05-13 Arma Corp Self-synchronously controlled induction motor follow-up apparatus
US2496809A (en) * 1941-02-10 1950-02-07 Sperry Corp Radio controlled pilot system
US2514555A (en) * 1941-06-21 1950-07-11 Bendix Aviat Corp Electric motor control system
US2548884A (en) * 1941-11-01 1951-04-17 Sperry Corp Remote positional control mechanism
US2526665A (en) * 1942-01-24 1950-10-24 Sperry Corp Positional control system
US2423337A (en) * 1942-05-25 1947-07-01 Sperry Gyroscope Co Inc Radio controlled pilot system
US2417868A (en) * 1943-05-31 1947-03-25 Askania Regulator Co Electric motor speed control circuits
US2471422A (en) * 1943-07-09 1949-05-31 Sperry Corp Position and speed control system
US2425317A (en) * 1943-07-13 1947-08-12 Sperry Gyroscope Co Inc Prediction apparatus
US2506798A (en) * 1943-08-06 1950-05-09 Barber Colman Co Stabilized power actuator and method of operating same
US2847867A (en) * 1943-08-24 1958-08-19 Remco Electronic Inc Follow-up device
US2503346A (en) * 1943-10-01 1950-04-11 Smith & Sons Ltd S Automatic stabilizing control system
US2512665A (en) * 1943-10-18 1950-06-27 Smith & Sons Ltd S Electric motor control system
US2689333A (en) * 1944-03-31 1954-09-14 Us Navy Magnetic stabilization system
US2478203A (en) * 1944-04-08 1949-08-09 Sperry Corp Follow-up motor control circuit
US2875575A (en) * 1944-10-30 1959-03-03 Bendix Aviat Corp Control systems and apparatus for the power units of aircraft
US2572986A (en) * 1945-03-22 1951-10-30 Chance Britton Radar tracking system
US2541666A (en) * 1945-05-12 1951-02-13 Curtiss Wright Corp Control system
US2464362A (en) * 1945-06-28 1949-03-15 Westinghouse Electric Corp Servomotor damper
US2478279A (en) * 1945-07-07 1949-08-09 Curtiss Wright Corp Control system
US2513537A (en) * 1945-07-20 1950-07-04 Williams Frederic Calland Electric integrator using a motor with velocity feedback
US2567202A (en) * 1945-07-31 1951-09-11 Sperry Corp Eddy-current generator and control circuits
US2497216A (en) * 1945-09-28 1950-02-14 Rca Corp Servo system derivative generator
US2444813A (en) * 1945-11-02 1948-07-06 Arma Corp Servo control system
US2538494A (en) * 1946-01-15 1951-01-16 Rca Corp Servo control amplifier
US2488734A (en) * 1946-03-07 1949-11-22 Research Corp Dynamo transformer
US2545405A (en) * 1946-03-13 1951-03-13 Askania Regulator Co Electrical motor control system
US2574104A (en) * 1946-07-01 1951-11-06 Ampro Corp Position and movement reproducing apparatus
US2484089A (en) * 1946-12-31 1949-10-11 Rca Corp Motor speed control
US2642554A (en) * 1947-01-23 1953-06-16 Bendix Aviat Corp Automatic steering system
US2537027A (en) * 1947-02-08 1951-01-09 Duncan Electric Mfg Co Follow-up apparatus
US2595868A (en) * 1947-05-05 1952-05-06 Smith & Sons Ltd S Automatic control system
US2604615A (en) * 1947-05-13 1952-07-22 Bendix Aviat Corp Engine speed control
US2453451A (en) * 1947-05-21 1948-11-09 Collins Radio Co Voltage regulator system
US2492392A (en) * 1947-05-21 1949-12-27 Collins Radio Co Remotely tuned radio apparatus and the like
US2620463A (en) * 1947-06-12 1952-12-02 Smith & Sons Ltd S Automatic control system
US2650338A (en) * 1948-02-16 1953-08-25 Smith & Sons Ltd S Automatic aircraft control system
US2700888A (en) * 1948-04-27 1955-02-01 Walter A Good Simulator for predicting the behavior of a roll-stabilized vehicle in flight
US2489184A (en) * 1948-05-10 1949-11-22 Dynamatic Corp Electronic governing apparatus for electric machinery
US2664530A (en) * 1948-07-17 1953-12-29 Gen Electric Autopilot control system
US2582305A (en) * 1948-07-17 1952-01-15 Gen Electric Airplane maneuvering system
US2694900A (en) * 1948-07-27 1954-11-23 Bendix Aviat Corp Aircraft engine power control to maintain selected combustion chamber temperature and engine speed conditions
US2686021A (en) * 1948-09-10 1954-08-10 Sperry Corp Aircraft automatic pilot turn control
US2630282A (en) * 1948-09-10 1953-03-03 Sperry Corp Aircraft automatic pilot turn control system
US2646924A (en) * 1948-11-29 1953-07-28 Honeywell Regulator Co Computer for estimated time of arrival
US2813236A (en) * 1949-01-14 1957-11-12 Sperry Rand Corp Control system for electric servomotors
US2605452A (en) * 1949-03-04 1952-07-29 Edward P Ney Stabilizing system using an amplidyne
US2651014A (en) * 1949-03-24 1953-09-01 Honeywell Regulator Co Electronic amplifier with double frequency discriminator
US2695981A (en) * 1949-08-13 1954-11-30 Republic Flow Meters Co Follow-up type of measuring apparatus
US2795748A (en) * 1952-07-16 1957-06-11 Thompson Prod Inc Automatic speed control system using variable transmission
US2795747A (en) * 1952-07-16 1957-06-11 Thompson Prod Inc Automatic speed and stabilizing control using variable transmission
US2727201A (en) * 1952-07-29 1955-12-13 Gen Electric Motor control system
US2769122A (en) * 1953-04-01 1956-10-30 Bendix Aviat Corp Self-balancing servo system
US2751535A (en) * 1953-06-18 1956-06-19 Alexander H Kuhnel Position control system
US2783427A (en) * 1953-07-10 1957-02-26 W L Maxson Corp Motor control systems
US2832028A (en) * 1953-10-09 1958-04-22 Sperry Gyroscope Co Ltd Positional control systems
US2766413A (en) * 1954-02-10 1956-10-09 Allen E Young Position-sensitive probe circuit
US2776397A (en) * 1954-03-04 1957-01-01 Bendix Aviat Corp Temperature compensated motor control system
US2832020A (en) * 1954-04-12 1958-04-22 Northrop Aircraft Inc Synchro system and quadrature voltage eliminator therefor
US2885614A (en) * 1954-05-03 1959-05-05 United Aircraft Corp Servosystem angular motion transmitting apparatus
US2802160A (en) * 1954-11-09 1957-08-06 Gen Electric Intermediate zone locating servosystem
US2810103A (en) * 1954-12-13 1957-10-15 Cook Electric Co Multiple mode servomechanism
US2869059A (en) * 1954-12-13 1959-01-13 Cook Electric Co Follow-up control systems
US2843882A (en) * 1955-06-08 1958-07-22 Us Rubber Co Evener
US2946942A (en) * 1955-07-01 1960-07-26 Amcel Propulsion Inc Thyratron control system
US2881379A (en) * 1955-07-26 1959-04-07 Jr Benjamin F Logan Velocity servosystem with signal quadrature component suppression
US2829323A (en) * 1955-07-29 1958-04-01 Digital Control Systems Inc Rate digital control system
US2825861A (en) * 1955-12-22 1958-03-04 Emerson Radio & Phonograph Cor Integrating servo mechanism
US2859397A (en) * 1955-12-28 1958-11-04 Gen Electric Feedback type control system
US3064173A (en) * 1956-05-18 1962-11-13 Celanese Corp Speed slaving method and apparatus
US2896142A (en) * 1956-12-12 1959-07-21 Bosch Arma Corp Servo controller
US3017556A (en) * 1957-03-18 1962-01-16 Republic Flow Meters Co Electrical servosystem control circuit
US2934689A (en) * 1957-11-22 1960-04-26 Gen Precision Inc Servo systems and quadrature signal filter therefor
US2939061A (en) * 1957-11-29 1960-05-31 American Machine & Metals Indicator servosystem
US2965828A (en) * 1958-07-24 1960-12-20 Gen Precision Inc Servo damping mechanism
US3100277A (en) * 1958-09-08 1963-08-06 Stuart N Mccullough Switching servo system with anti-hunt feedback
US2996650A (en) * 1959-05-12 1961-08-15 Gen Precision Inc Servosystem with damping which decreases with servomotor speed
US3108212A (en) * 1960-02-29 1963-10-22 Singer Inc H R B Duty-factor controlled motor
US3172025A (en) * 1960-05-16 1965-03-02 Gen Precision Inc Linear servo mechanism
US3100858A (en) * 1960-08-12 1963-08-13 Sperry Rand Corp Pressure rebalancing and measuring servosystem
US3079539A (en) * 1960-08-15 1963-02-26 Fritz A Guerth Servosystem and pulse type amplifier

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