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GB662844A - Control system - Google Patents

Control system

Info

Publication number
GB662844A
GB662844A GB3038/47A GB303847A GB662844A GB 662844 A GB662844 A GB 662844A GB 3038/47 A GB3038/47 A GB 3038/47A GB 303847 A GB303847 A GB 303847A GB 662844 A GB662844 A GB 662844A
Authority
GB
United Kingdom
Prior art keywords
signal
servomotor
follow
deviation
bridge
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
GB3038/47A
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 GB662844A publication Critical patent/GB662844A/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

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 Or Direction (AREA)
  • Manipulator (AREA)

Abstract

662,844. Automatic control systems. BENDIX AVIATION CORPORATION. Jan. 31, 1947 [Feb. 18, 1946], No. 3038/47. Class 38 (iv). An electrical control signal is produced by a normally balanced bridge which is rendered unbalanced by the change in temperature of a second bridge forming one of its arms and to which the initiating signal is applied. In a craft control system, as shown, Fig. 4, which is an improvement on that described in Specification 611,226, the deviation signal derived at 11 is applied through the amplifier 16 to the servomotor 42 of the control surface 10, and to stabilize the system at the correct datum, an additional signal is applied, with the feed-back signal, to the servomotor through the valve 82 and the time-delay, heat-responsive bridges respectively composed of equal resistors 68, 69, 70, 71 and 73, 74, 75, 76. The heat responsive bridges, together with the resistors 60, 61 form a further normally balanced bridge to which is applied the followup signal and which unbalances in a sense dependent on the sense of the follow-up signal if the follow-up signal is persistant, to provide the additional automatic trim control signal. In a further embodiment, Fig. 5 (not shown), heating is prevented in a control system as in Fig. 4 by the application of the deviation signal to the time-delay bridge circuit, the output of which is applied, with the deviation and follow-up signals to the servomotor. Specifications 662,831 and 662,845, [Group XXXVI], are referred to.
GB3038/47A 1946-02-18 1947-01-31 Control system Expired GB662844A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US662844XA 1946-02-18 1946-02-18

Publications (1)

Publication Number Publication Date
GB662844A true GB662844A (en) 1951-12-12

Family

ID=22068520

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3038/47A Expired GB662844A (en) 1946-02-18 1947-01-31 Control system

Country Status (1)

Country Link
GB (1) GB662844A (en)

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