US2371415A - Remote control circuit - Google Patents

Remote control circuit Download PDF

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Publication number
US2371415A
US2371415A US467453A US46745342A US2371415A US 2371415 A US2371415 A US 2371415A US 467453 A US467453 A US 467453A US 46745342 A US46745342 A US 46745342A US 2371415 A US2371415 A US 2371415A
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control
motor
signal
positive
negative
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US467453A
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William A Tolson
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RCA Corp
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RCA Corp
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    • GPHYSICS
    • G08SIGNALLING
    • G08CTRANSMISSION SYSTEMS FOR MEASURED VALUES, CONTROL OR SIMILAR SIGNALS
    • G08C19/00Electric signal transmission systems
    • G08C19/16Electric signal transmission systems in which transmission is by pulses
    • G08C19/22Electric signal transmission systems in which transmission is by pulses by varying the duration of individual pulses

Description

March 13, 19.45. w, A TOLSON I 2,371,415'
REMOTE CONTROL CIRCUIT Filed Nav. 3o, 1942 Moos cue/eem' T5 I W, f/ 2590 nnentor BH @w (ttorneg Patented Mar. 13, 1945 REMOTE CONTROL CIRCUIT William A. Tolson, Princeton,
N. J., assignor to Radio Corporation of America, a corporation of Delaware Application November 30, 1942, Serial No. 467,453
Claims.
This invention relates to remote control systems, and more particularly to an improved method of and means for controlling the position of a movable object by means of electrical signals. Frequently the control signal channel for such a system includes a radio link or other transmission means subject to interference from external sources, which may Vderange the operation of the system, causing false response or failure.
AAccordingly, it is the principal object of the present invention to provide an improved method of and means for remote control, avoiding to a large extent the deleterious effects of interference with the controlsignals.
Another object is to provide a method of and means for utilizing pulse signals for remote control.
A further object is to utilize said pulse signals so as to respond to the timing, rather than to the amplitudes or wave shapes of the pulses.
These and other objects will become apparent to those skilled in the art upon consideration of the following description, with reference to the accompanying drawing, of which Fig.A 1 is a schematic diagram of receiver system embody- .ing'the invention, Fig. 2 is a schematic diagram of a system for generating control signals of the type used in the practice of the invention, Fig. 3 is a group of graphical representations of wave shapes of the voltages occurring at various points in the circuit during operation, and Fig.v4 is a modified transmitter system.
It has been found that in the control of tele- 14Vlvision receivers, by means of pulse signals, the effects of interference are minimized by virtue of the fact that the essence of the control signals lies in their timing, rather than in their amplitude or exact wave shape. This effect is taken advantage of in the system described below, in that control is accomplished by varying the durations of alternate positive and negative pulses.
Referring first to Fig. 3, the normal condition is that in which the net torque output of thel system is zero. The controlsignal input is a square wave having positive and negative loops of equal time duration. Under plus control the net torque is positive. clockwise. for example. The corresponding control signal input is a wave with positive loops of less duration than the negative loops. Conversely, the signal for minus control, or counterclockwise torque, has positive loops of greater duration than the negative loops.
Referring to Fig. 1. a tube I. is connected as a phase inverter. The output of the phase inverter is applied in push-pull to a pair of tubes 3 and 5 which are connected as yamplifiers and are coupled directly to the control grids of a pair of power tubes 1 and 9. The tubes 3 and 5 are self biased by the grid leaks 6 and capacitors 8. The anode circuits of the power tubes 1 and 9 are connected to direct current motor armatures II and I3 which are mounted on a single shaft I5 and are provided with a common field winding I1. The two armatures are connected in bucking relation to each other, so that the anode current of the tube 1 tends to produce rotation of the shaft I5 in the opposite direction to that produced by the anode current in the tube 9. 'I'he shaft I5 is mechanically connected to a con trol shaft I8 which provides the mechanical output of the system. The connection between the shafts I5 and IS may include a torque amplier I6, of any conventional design. A double potentiometer 2| is connected in a bridge circuit across a D.C. source 23. The moveable arms 25 and 21 are mechanically connected to the shaft I9 and electrically connected to the screen grids of the tubes 1 and 9 respectively. The armatures II and I'3 are shunted by a pair of capacitors 29 and 3I respectively.
'I'he operation of the system of Fig. 1 is as follows:
With a signal input such as that designated as "normal in Fig. 3, theoutputs of the tube I comprise rectangular Waves of equal durations and opposite polarities. The bias at the grids of the tubes 3 and 5 is set substantially at the input voltage peaks, due to charging of the coupling capacitors by grid current on the positive swings and discharges of the coupling capacitors through the grid leaks on the negative swings. :Thus the positive pulse loops are amplified by the tube 5, and the negative loops by the tube 3, providing similar voltage pulses on the grids of the tubes 1 and 9. `'Ihese pulses are of suflicient amplitude to out off the anode currents on the negative swings, so that the tubes 1 and 9 are alternately conductive during equal periods as illustrated by conditions shown in Fig. 3. When the input signal comprises positive pulses of shorter durations than the negative pulses as illustrated by the pulse control of Fig. 3, the periods during which the tube 1 is conductive are shorter than those during .which the tube 9 conducts. The average current through the armature winding II is thus less than the average current through the armature I3 and 'the motor shaft I5 is rotated in a clockwise direction. The capacitors 29 and 3l serve to smooth out the pulses of the anode currents into comparatively steady direct currents through the armatures. 'I'he rotation ofthe shaft I5 and with it the shaft I9 operates the potentiometer 2| to increase the screen grid voltage on the tube I simultaneously decreasing the voltage on the screen of the tube 9. This increases the amplitudes of the pulses in the output of the tube 1 and decreases the output of the tube 8. This operation continues until the average currents through the two armatures are equal, whereupon the net torque on the shaft I5 becomes zero. This condition is maintained as long as the input signal remains unchanged. The operation of this system under the uminus control conditions is identical with that described above, but in the wrapped around the drum. A slip ring 4I is provided at one end of the drum 33 and is connected to or constructed integrally with the sheet 35. A second slip ring 42 at the other end is connected to the sheet 40. Brushes 43 and 44 are supported in engagement with the slip rings 4I and 42 respectively. A contact 45 is supported on the pivot 41 and connected to a control lever 49. Direct current sources 5I are connected to the brushes 4 3 and'44 in opposite polarities and to one side of the signal output circuit. The contact 45 is connected to the other side of the output circuit. The operationv of the signal generating device of Fig. 2 is as follows:
As the drum 33 is rotated continuously by the motor 35, the contact 45 engages the sheets 39 and 40, providing alternate positive and negative pulses in the signal output circuit.
'I'he ratio of the positive pulse duration timev to the negative pulse duration time is a function of the position of the contact 45 with respect to the drum 43. If the contact 45 is moved toward its right hand position, the negative pulses applied to the signal output circuit have a duration time longer than that of the positive pulses as illustrated under the plus control condition in Fig. 3. Similarly, if the contact 45 is moved toward the left minus control signals are produced.
Fig. 4 illustrates a modified signal generator device comprising a drum 33 similar to that of Fig. 2 provided with a single triangular sheet 39 covering one half of its surface. A single D.-C. source 5I is switched on and off during rotation of the drum 35, the ratio of the on period to the of! period being a function of the position of the control lever. A capacitor 53 may be provided in the signal output circuit. This shifts the zero axis of the signal to a point between the upper and lower loops of the wave, providing signals like those illustrated in Fig. 3. The capacitor 53 may be omitted if a receiver system like that illustrated in Fig. 1 is used` since the coupling capacitors 8 between the phase inverter I and the tubes 3 and 5 will provide the same effect.
Thus the invention has been described as an improved remote control system employing pulse signals of variable duration times to achieve freedom from the effects of interference. One
embodiment of the invention has been described including a, motor with a. double armaturewinding energized through negative peak limiting amplifiers and driving a double potentiometer to balance the energization of the two armatura by diilerentially controlling the gains oi' the amplifiers. In some instances, it may be desirableto substitute equivalent means for practicing the invention, such as, for example, a motor provided with two flelds and a single armature. It is also to be noted that the follow-up connection, comprising the potentiometer 2| and the associated circuits, may be omitted. 'I'hen the motor will be energized to provide a torque corresponding in magnitude and direction to the position of the controller, instead of running to some corresponding position and stopping.
I claim as my invention:
1. The method of operating an electric motor in response to variation in the position of s control device comprising the steps oi deriving a voltage of rectangular wave form with positive loops related in duration time to the negative loops of said wave as a function of the position of said control member, deriving from said voltage a second voltage inverted in polaritywith respect to said first voltage, energizing said motor to produce torque in one direction in response-to said first voltage and energizing said motor to produce torque in the opposite direction in response to said second voltage, whereby said motor produces an average torque related to the diierence between the duration times of said positive loops and the duration times of said negative loops.
2. The method of controlling an electric motor comprising the steps of producing a control signal comprising a wave of substantially constant repetition period and variable duration period, deriving therefrom a second signal similar ,to said control `signal but inverted in polarity, cutting otr the negative loops and integrating the positive loops of both of saidv signals. energizing said motor to produce torque in one direction in response to the iirst of said integratedsignals, and energizing said motor to produce torque inthe opposite direction in response to the second of Saidintegrated signals.
3. The method of controlling a motor in response to variations in the position of a control device including the steps of deriving a control signal comprising impulses of constant repetition period and of duration period variable in response to the position of said control device, deriving from said control signal a second signal similar to said control signal but inverted in polarity, cutting oil the negative loopsof both of said signals, amplifying the positive loops of said signals separately, integrating said ampliiled signals, energizing said motor to produce torque in one direction in response to one of saidv amplined and integrated signals, simultaneously energizing said motor to produce torque in the opposite direction in response tothe other of said amplified and integrated signals, and difierentially varying the amplification of said signals in response to the angular position of the shaft of said motor.
4. A remote control system including an electric. motor provided with differentially operative power input circuits, amplifiers connected to supply power to each of said circuits respectively, said impliners being biased to conduct only in response to positive signal impulsesl and to cut off in response to negative signal impulses, a. signal input circuit, phase inverter means connected I nating voltage Wave with positive between said signal input circuit and the input circuits of said ampliers, and means for difierentially varying the gains of said amplifiers in response to the angular position of the output shaft oi' said motor.
5. A system for operating an electric motor in response to variation in the position of a control device, including means for producing an alterloops related in duration time to the negative loops o! said l0 wave as a predetermined function of the position oi' said control member, amplers connecte to supply power to said motor so as to produce torque in respectively opposite directions of rotation. means for applying said voltage wave in one polarity to the input circuit of one of said ampliilers in the opposite polarity to the input circuit of the other of said amplifiers.
WILLIAM A. TOLSON.
US467453A 1942-11-30 1942-11-30 Remote control circuit Expired - Lifetime US2371415A (en)

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Cited By (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2419292A (en) * 1947-04-22 System fob transmitting two
US2451129A (en) * 1944-03-31 1948-10-12 Bristol Company Telemetering apparatus of the impulse-duration class
US2454045A (en) * 1945-05-16 1948-11-16 Bell Telephone Labor Inc Amplifier
US2472535A (en) * 1943-04-29 1949-06-07 Pye Ltd Electric remote-control or indicating system
US2475363A (en) * 1945-04-10 1949-07-05 Raytheon Mfg Co System for echo ranging
US2486935A (en) * 1946-07-24 1949-11-01 Stewart Warner Corp Voltage controlled proportional positioning apparatus
US2524665A (en) * 1947-10-25 1950-10-03 Bailey Meter Co Telemetric system
US2525696A (en) * 1946-10-15 1950-10-10 Eli M Lurie Volume control arrangement
US2534712A (en) * 1945-11-30 1950-12-19 John W Gray Apparatus for measuring air speed
US2539525A (en) * 1948-07-03 1951-01-30 John J Root Servo mechanism
US2557581A (en) * 1947-02-15 1951-06-19 Rock Ola Mfg Corp Remote control system
US2565213A (en) * 1947-02-08 1951-08-21 Louis F Falkenstein Course or condition maintaining mechanism
US2565540A (en) * 1945-01-27 1951-08-28 Everard M Williams Proportional control system
US2567862A (en) * 1945-05-17 1951-09-11 Stanley N Van Voorhis Communication system
US2568241A (en) * 1944-11-08 1951-09-18 Philip W Martin Apparatus for logging
US2588102A (en) * 1948-10-22 1952-03-04 Francisco A Forero Liquid level signaling apparatus
US2598937A (en) * 1950-04-24 1952-06-03 North American Aviation Inc Curve follower
US2609526A (en) * 1948-02-10 1952-09-02 Louis F Falkenstein Course or condition maintenance
US2634414A (en) * 1945-08-28 1953-04-07 Gordon W Andrew Proportional control
US2707143A (en) * 1949-06-16 1955-04-26 Thompson Prod Inc Graphic recorder
US2720618A (en) * 1951-11-28 1955-10-11 Honeywell Regulator Co Balancing circuits for electric motor control system
US2721989A (en) * 1949-11-29 1955-10-25 United Shoe Machinery Corp Recording magnitudes in ratio form
US2808550A (en) * 1953-10-12 1957-10-01 Collins Radio Co Servosystem including phase sensitive amplifier
US2816860A (en) * 1945-04-14 1957-12-17 Volney C Wilson Means for controlling a nuclear reactor
US2863113A (en) * 1957-02-13 1958-12-02 Honeywell Regulator Co Current control apparatus
US2980903A (en) * 1948-03-19 1961-04-18 Goodyear Aircraft Corp Radar-command system of time coded pulses
US3127553A (en) * 1959-09-11 1964-03-31 Prec Control Corp Control system for energizing a directcurrent load from an alternatingcurrent source

Cited By (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2419292A (en) * 1947-04-22 System fob transmitting two
US2472535A (en) * 1943-04-29 1949-06-07 Pye Ltd Electric remote-control or indicating system
US2451129A (en) * 1944-03-31 1948-10-12 Bristol Company Telemetering apparatus of the impulse-duration class
US2568241A (en) * 1944-11-08 1951-09-18 Philip W Martin Apparatus for logging
US2565540A (en) * 1945-01-27 1951-08-28 Everard M Williams Proportional control system
US2475363A (en) * 1945-04-10 1949-07-05 Raytheon Mfg Co System for echo ranging
US2816860A (en) * 1945-04-14 1957-12-17 Volney C Wilson Means for controlling a nuclear reactor
US2454045A (en) * 1945-05-16 1948-11-16 Bell Telephone Labor Inc Amplifier
US2567862A (en) * 1945-05-17 1951-09-11 Stanley N Van Voorhis Communication system
US2634414A (en) * 1945-08-28 1953-04-07 Gordon W Andrew Proportional control
US2534712A (en) * 1945-11-30 1950-12-19 John W Gray Apparatus for measuring air speed
US2486935A (en) * 1946-07-24 1949-11-01 Stewart Warner Corp Voltage controlled proportional positioning apparatus
US2525696A (en) * 1946-10-15 1950-10-10 Eli M Lurie Volume control arrangement
US2565213A (en) * 1947-02-08 1951-08-21 Louis F Falkenstein Course or condition maintaining mechanism
US2557581A (en) * 1947-02-15 1951-06-19 Rock Ola Mfg Corp Remote control system
US2524665A (en) * 1947-10-25 1950-10-03 Bailey Meter Co Telemetric system
US2609526A (en) * 1948-02-10 1952-09-02 Louis F Falkenstein Course or condition maintenance
US2980903A (en) * 1948-03-19 1961-04-18 Goodyear Aircraft Corp Radar-command system of time coded pulses
US2539525A (en) * 1948-07-03 1951-01-30 John J Root Servo mechanism
US2588102A (en) * 1948-10-22 1952-03-04 Francisco A Forero Liquid level signaling apparatus
US2707143A (en) * 1949-06-16 1955-04-26 Thompson Prod Inc Graphic recorder
US2721989A (en) * 1949-11-29 1955-10-25 United Shoe Machinery Corp Recording magnitudes in ratio form
US2598937A (en) * 1950-04-24 1952-06-03 North American Aviation Inc Curve follower
US2720618A (en) * 1951-11-28 1955-10-11 Honeywell Regulator Co Balancing circuits for electric motor control system
US2808550A (en) * 1953-10-12 1957-10-01 Collins Radio Co Servosystem including phase sensitive amplifier
US2863113A (en) * 1957-02-13 1958-12-02 Honeywell Regulator Co Current control apparatus
US3127553A (en) * 1959-09-11 1964-03-31 Prec Control Corp Control system for energizing a directcurrent load from an alternatingcurrent source

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