GB666272A - Improvements in or relating to automatic control systems for aircraft - Google Patents

Improvements in or relating to automatic control systems for aircraft

Info

Publication number
GB666272A
GB666272A GB8216/49A GB821649A GB666272A GB 666272 A GB666272 A GB 666272A GB 8216/49 A GB8216/49 A GB 8216/49A GB 821649 A GB821649 A GB 821649A GB 666272 A GB666272 A GB 666272A
Authority
GB
United Kingdom
Prior art keywords
aircraft
control systems
automatic control
relating
march
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
GB8216/49A
Inventor
Frederick William Meredith
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 GB8216/49A priority Critical patent/GB666272A/en
Publication of GB666272A publication Critical patent/GB666272A/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
    • G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0816—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability
    • 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
    • G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0858—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft specially adapted for vertical take-off of aircraft

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)
  • Feedback Control In General (AREA)

Abstract

666,272. Automatic aircraft control systems. SMITH & SONS (ENGLAND), Ltd. March 23, 1950 [March 25, 1949], No. 8216/49. Drawings to Specification. Class 38 (iv). In an automatic control system such as that described in Specification 611,037, in which the aircraft is controlled in accordance with the deviation plus rate of turn from its datum attitude, the D.C. rate of turn signal is modified to attenuate its higher-frequency Fourier components by applying it to a series R.C. network and using the signal voltage across the capacitor.
GB8216/49A 1949-03-25 1949-03-25 Improvements in or relating to automatic control systems for aircraft Expired GB666272A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB8216/49A GB666272A (en) 1949-03-25 1949-03-25 Improvements in or relating to automatic control systems for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8216/49A GB666272A (en) 1949-03-25 1949-03-25 Improvements in or relating to automatic control systems for aircraft

Publications (1)

Publication Number Publication Date
GB666272A true GB666272A (en) 1952-02-06

Family

ID=9848144

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8216/49A Expired GB666272A (en) 1949-03-25 1949-03-25 Improvements in or relating to automatic control systems for aircraft

Country Status (1)

Country Link
GB (1) GB666272A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3079107A (en) * 1958-03-03 1963-02-26 Motorola Inc System for controlling an aircraft from a magnetic sensor

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3079107A (en) * 1958-03-03 1963-02-26 Motorola Inc System for controlling an aircraft from a magnetic sensor

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