GB662859A - Automatic pilot - Google Patents

Automatic pilot

Info

Publication number
GB662859A
GB662859A GB13637/50A GB1363750A GB662859A GB 662859 A GB662859 A GB 662859A GB 13637/50 A GB13637/50 A GB 13637/50A GB 1363750 A GB1363750 A GB 1363750A GB 662859 A GB662859 A GB 662859A
Authority
GB
United Kingdom
Prior art keywords
craft
signal generator
servomotor
induction signal
group
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
GB13637/50A
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.)
Bendix Aviation Corp
Original Assignee
Bendix Aviation Corp
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 Bendix Aviation Corp filed Critical Bendix Aviation Corp
Publication of GB662859A publication Critical patent/GB662859A/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
    • G05D1/085—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability to ensure coordination between different movements

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)
  • Electric Propulsion And Braking For Vehicles (AREA)
  • Power Steering Mechanism (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Abstract

662,859. Automatic steering control systems. BENDIX AVIATION CORPORATION. Nov. 17, 1944 [Dec. 31, 1943], No. 13637/50. Divided out of 662,831. Drawings to Specification. Class 38 (iv). The Specification describes the same apparatus as that described in 662,831, but the claims are directed to the feature of controlling the craft control surfaces directly by the power of an electrical servomotor through a purely mechanical linkage. The operation of the servomotor is controlled by two electrical signals, one produced by an induction signal generator responsive to deviation of the craft from a prescribed strictive or attitude and the other by another induction signal generator in response to displacement of the control surface with respect to the craft. Specifications 550,399, 550,779, 565,277, [all in Group XXXVIII], 592,394, [Group XXXVI], 662,854 and 662,855 are referred to.
GB13637/50A 1943-12-31 1944-11-17 Automatic pilot Expired GB662859A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US662859XA 1943-12-31 1943-12-31

Publications (1)

Publication Number Publication Date
GB662859A true GB662859A (en) 1951-12-12

Family

ID=22068542

Family Applications (1)

Application Number Title Priority Date Filing Date
GB13637/50A Expired GB662859A (en) 1943-12-31 1944-11-17 Automatic pilot

Country Status (1)

Country Link
GB (1) GB662859A (en)

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