GB931073A - Aircraft attitude control device - Google Patents

Aircraft attitude control device

Info

Publication number
GB931073A
GB931073A GB26670/59A GB2667059A GB931073A GB 931073 A GB931073 A GB 931073A GB 26670/59 A GB26670/59 A GB 26670/59A GB 2667059 A GB2667059 A GB 2667059A GB 931073 A GB931073 A GB 931073A
Authority
GB
United Kingdom
Prior art keywords
signals
attitude reference
aircraft
amplifier
attitude
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
GB26670/59A
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.)
PE Manufacturing GmbH
Original Assignee
Bodenseewerk Perkin Elmer and Co GmbH
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 Bodenseewerk Perkin Elmer and Co GmbH filed Critical Bodenseewerk Perkin Elmer and Co GmbH
Publication of GB931073A publication Critical patent/GB931073A/en
Expired legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/10—Simultaneous control of position or course in three dimensions
    • G05D1/107—Simultaneous control of position or course in three dimensions specially adapted for missiles

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

931,073. Automatic steering control. BODENSEWERK PERKIN-ELMER E CO. G.m.b.H. Aug. 5, 1959 [Aug. 14, 1958], No. 26670/59. Drawings to Specification. Class 38 (4). In an aircraft automatic pilot in which signals from an attitude reference fixed in space control the attitude of the aircraft through a servosystem, turns are effected by applying a signal directly to the servo-system, the signals from the attitude reference, which oppose the turn for a time, being reduced to zero after a delay period. As described, signals from an attitude reference are applied through an electric amplifier to operate an aircraft control surface, followup signals being fed back to the amplifier from a potentiometer operated with the control surface. Turns are produced by applying signals directly to the amplifier, and the attitude reference is automatically adjusted by an electric motor controlled by signals from the attitude reference so that these signals are reduced to zero after a delay period.
GB26670/59A 1958-08-14 1959-08-05 Aircraft attitude control device Expired GB931073A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DEM38630A DE1078449B (en) 1958-08-14 1958-08-14 Device for the self-control of flight bodies

Publications (1)

Publication Number Publication Date
GB931073A true GB931073A (en) 1963-07-10

Family

ID=7303157

Family Applications (1)

Application Number Title Priority Date Filing Date
GB26670/59A Expired GB931073A (en) 1958-08-14 1959-08-05 Aircraft attitude control device

Country Status (2)

Country Link
DE (1) DE1078449B (en)
GB (1) GB931073A (en)

Also Published As

Publication number Publication date
DE1078449B (en) 1960-03-24

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