GB845600A - Improvements in or relating to servo systems - Google Patents

Improvements in or relating to servo systems

Info

Publication number
GB845600A
GB845600A GB33448/57A GB3344857A GB845600A GB 845600 A GB845600 A GB 845600A GB 33448/57 A GB33448/57 A GB 33448/57A GB 3344857 A GB3344857 A GB 3344857A GB 845600 A GB845600 A GB 845600A
Authority
GB
United Kingdom
Prior art keywords
amplifier
limiter
phase
signal
control
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
GB33448/57A
Inventor
Derek Shave
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.)
S Smith and Sons Ltd
S Smith and Sons England Ltd
Original Assignee
S Smith and Sons Ltd
S Smith and Sons England Ltd
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 S Smith and Sons Ltd, S Smith and Sons England Ltd filed Critical S Smith and Sons Ltd
Priority to GB33448/57A priority Critical patent/GB845600A/en
Publication of GB845600A publication Critical patent/GB845600A/en
Expired legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/08Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0816Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B9/00Servomotors with follow-up action, e.g. obtained by feed-back control, i.e. in which the position of the actuated member conforms with that of the controlling member

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Abstract

845,600. Automatic control systems. SMITH & SONS (ENGLAND) Ltd., S. Oct. 27, 1958 [Oct. 25, 1957], No. 33448/57. Drawings to Specification. Class 38 (4). In a closed loop control system for positioning an object, the control signal is applied through an amplifier, phase advancer, limiter, and phase retarder, arranged in cascade, to control a servomotor. In the arrangement described an electric signal corresponding to a desired attitude of an aircraft is applied, in opposition with a signal derived from a position gyro on the craft, to an amplifier feeding a phase advance network, a limiter and a phase lag network in cascade. The overall transfer function of the three latter units is unity unless the signal exceeds the limit of the limiter, in which case the arrangement improves stability. The output signal is applied through a second amplifier to energize an electro-hydraulic valve controlling an hydraulic jack which operates a control surface to correct the attitude of the aircraft. A position feedback signal derived from operation of the jack is applied to the input of the second amplifier.
GB33448/57A 1957-10-25 1957-10-25 Improvements in or relating to servo systems Expired GB845600A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB33448/57A GB845600A (en) 1957-10-25 1957-10-25 Improvements in or relating to servo systems

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB33448/57A GB845600A (en) 1957-10-25 1957-10-25 Improvements in or relating to servo systems

Publications (1)

Publication Number Publication Date
GB845600A true GB845600A (en) 1960-08-24

Family

ID=10353086

Family Applications (1)

Application Number Title Priority Date Filing Date
GB33448/57A Expired GB845600A (en) 1957-10-25 1957-10-25 Improvements in or relating to servo systems

Country Status (1)

Country Link
GB (1) GB845600A (en)

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