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GB612307A - Improvements in or relating to control systems - Google Patents

Improvements in or relating to control systems

Info

Publication number
GB612307A
GB612307A GB18689/44A GB1868944A GB612307A GB 612307 A GB612307 A GB 612307A GB 18689/44 A GB18689/44 A GB 18689/44A GB 1868944 A GB1868944 A GB 1868944A GB 612307 A GB612307 A GB 612307A
Authority
GB
United Kingdom
Prior art keywords
gyro
rotor
voltage
phase
source
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
GB18689/44A
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 GB612307A publication Critical patent/GB612307A/en
Expired legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C19/00Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
    • G01C19/02Rotary gyroscopes
    • G01C19/34Rotary gyroscopes for indicating a direction in the horizontal plane, e.g. directional gyroscopes
    • G01C19/36Rotary gyroscopes for indicating a direction in the horizontal plane, e.g. directional gyroscopes with north-seeking action by magnetic means, e.g. gyromagnetic compasses

Landscapes

  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Magnetic Bearings And Hydrostatic Bearings (AREA)
  • Control Of Electric Motors In General (AREA)

Abstract

612,307. Automatic control systems for gyroscopes. SPERRY GYROSCOPE CO., Inc. Sept. 29, 1944, No. 18689. Convention date, May 29, 1943. [Class 38 (iv)] [Also in Group XX] Alignment.-In a closed sequence control system for a variable, an A.C. signal in response to error starts an oscillator, the output of which controls servo-means effecting correction. In Fig. 1, a three-legged flux valve 1, pendulously supported (Fig. 2, not shown) on a craft, has exciting coils 2, energized from an alternating current source 5, and output coils 3 giving a voltage dependent on their position relative to the earth's field. The output from coils 3 is applied to the three-winding stator 6 of a remote Selsyn type unit, the rotor 8 of which is fixed to the vertical gimbal ring of a directional gyro (Fig. 2, not shown). The arrangement is such that the field produced by the stator 6 is fixed in space despite movement of the craft in azimuth and, provided the vertical ring of the gyro also remains fixed in space, no voltage is induced in rotor 8. Wander of the gyro, however, displaces rotor 8 relative to the stator field and a voltage proportional to the displacement is induced in rotor 8, its frequency being that of source 5 and its phase being dependent on the sense of the displacement. Rotor 8 forms with a condenser 9 a tuned circuit, the voltage across which is applied to the grid circuit of a pentode oscillator valve 11 which oscillates at half the frequency of source 5 whenever the rotor voltage is above a value corresponding to a small displacement of the gyro. The output from the oscillator when oscillating is independent of the voltage, but dependent on the phase of the rotor output and is amplified by a triode valve 22 and applied to a phase-sensitive double-diode valve 26, the anode currents of which, derived from source 5, selectively operate a two-way relay 28 according to the phase of the rotor voltage to energize an electromagnet 38 precessing the gyro in the appropriate sense for correction. In a modification, Figs. 3-5 (not shown), a single-legged flux valve is pendulously supported by the vertical ring of the gyro and the Selsyn type transmission dispensed with. Any suitable D.C. amplifier and torque motor may be substituted for relay 28 and electromagnet 38 respectively. If a two-phase torque motor is employed to precess the gyro, one phase may be controlled and the other supplied from a constant source such as source 5. Application of the invention to preventing wander of a gyro relative to a vertical reference is referred to. Specifications 600,189 and 604,907, [both in Group XXXVI], are referred to.
GB18689/44A 1943-05-29 1944-09-29 Improvements in or relating to control systems Expired GB612307A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US612307XA 1943-05-29 1943-05-29

Publications (1)

Publication Number Publication Date
GB612307A true GB612307A (en) 1948-11-11

Family

ID=22034472

Family Applications (1)

Application Number Title Priority Date Filing Date
GB18689/44A Expired GB612307A (en) 1943-05-29 1944-09-29 Improvements in or relating to control systems

Country Status (1)

Country Link
GB (1) GB612307A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9880027B2 (en) 2012-02-24 2018-01-30 Aisin Aw Co., Ltd. Resolver excitation apparatus

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9880027B2 (en) 2012-02-24 2018-01-30 Aisin Aw Co., Ltd. Resolver excitation apparatus
DE112012005053B4 (en) 2012-02-24 2019-05-16 Aisin Aw Co., Ltd. Resolver excitation device

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