GB616248A - Improvements in and relating to servo systems - Google Patents

Improvements in and relating to servo systems

Info

Publication number
GB616248A
GB616248A GB16527/44A GB1652744A GB616248A GB 616248 A GB616248 A GB 616248A GB 16527/44 A GB16527/44 A GB 16527/44A GB 1652744 A GB1652744 A GB 1652744A GB 616248 A GB616248 A GB 616248A
Authority
GB
United Kingdom
Prior art keywords
signal
error signal
amplifier
circuit
armature
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
GB16527/44A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Sperry Gyroscope Co Inc
Original Assignee
Sperry Gyroscope Co Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Sperry Gyroscope Co Inc filed Critical Sperry Gyroscope Co Inc
Publication of GB616248A publication Critical patent/GB616248A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • G05D3/14Control of position or direction using feedback using an analogue comparing device
    • G05D3/1436Control of position or direction using feedback using an analogue comparing device with fine or coarse devices

Abstract

616,248. Follow-up systems. SPERRY GYROSCOPE CO., Inc. Aug. 30, 1944, No. 16527. Convention date, Aug. 30, 1943. [Class 40 (i)] In a system in which an electric servomotor is controlled in accordance with the sense and magnitude of an error signal, the motor is a commutator motor in which the error signal controls the field excitation and variations of armature current resulting from the E.M.F. due to rotation of the armature are limited so that the torque remains proportional to the signal. As shown, Fig. 2, the error signal from coarse and fine selsyns which, owing to the presence of rectifier systems 37, 38 and 31, 32, are effective one at a time, is mixed with an anti-hunting signal derived from a tachometer generator 14 and differentiating circuit 54, 55 in a circuit involving a pair of twin triodes 42, 43 with an alternating plate supply to render the circuit phasesensitive. The resulting signal is amplified and applied to field windings 59, 60 of the servomotor. Variations of armature current are limited by a series resistor, capacitor or, as shown, inductor 62. In a modification, Fig. 3, the anti-hunting signal modulates, with the aid of a rectifier bridge 80 ... 82, a reference voltage 12 which is applied in series with the error voltage to a triode amplifier 66 feeding a push-pull amplifier 72, 73 similar to that in the system shown in Fig. 2. In another arrangement, Fig. 4 (not shown), the final amplifier is a single triode and the effect of the steady anode current is neutralized by an additional field winding carrying a direct current.
GB16527/44A 1943-08-30 1944-08-30 Improvements in and relating to servo systems Expired GB616248A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US616248XA 1961-04-10 1961-04-10

Publications (1)

Publication Number Publication Date
GB616248A true GB616248A (en) 1949-01-19

Family

ID=22037007

Family Applications (1)

Application Number Title Priority Date Filing Date
GB16527/44A Expired GB616248A (en) 1943-08-30 1944-08-30 Improvements in and relating to servo systems

Country Status (2)

Country Link
BE (1) BE616248A (en)
GB (1) GB616248A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2569571A (en) * 1944-05-05 1951-10-02 Sperry Corp Automatic gun control system
US2767580A (en) * 1952-02-26 1956-10-23 Bendix Aviat Corp Fluid flow indicating apparatus

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2569571A (en) * 1944-05-05 1951-10-02 Sperry Corp Automatic gun control system
US2767580A (en) * 1952-02-26 1956-10-23 Bendix Aviat Corp Fluid flow indicating apparatus

Also Published As

Publication number Publication date
BE616248A (en) 1962-07-31

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