GB1076262A - Control system for a vehicle, for example an aircraft - Google Patents

Control system for a vehicle, for example an aircraft

Info

Publication number
GB1076262A
GB1076262A GB39773/65A GB3977365A GB1076262A GB 1076262 A GB1076262 A GB 1076262A GB 39773/65 A GB39773/65 A GB 39773/65A GB 3977365 A GB3977365 A GB 3977365A GB 1076262 A GB1076262 A GB 1076262A
Authority
GB
United Kingdom
Prior art keywords
aircraft
ring
line
control
instrument
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
GB39773/65A
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.)
HERMAN CHRIS GALLAHER
JOHN JEROME GALLAHER
Original Assignee
HERMAN CHRIS GALLAHER
JOHN JEROME GALLAHER
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 HERMAN CHRIS GALLAHER, JOHN JEROME GALLAHER filed Critical HERMAN CHRIS GALLAHER
Priority to GB39773/65A priority Critical patent/GB1076262A/en
Publication of GB1076262A publication Critical patent/GB1076262A/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

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)
  • Toys (AREA)

Abstract

1,076,262. Aircraft control instruments. H. C. GALLAHER and J. J. GALLAHER. Sept. 17, 1965, No. 39773/65. Heading B7W. An instrument for assisting the roll control of an aeroplane comprises a ring 26 with bank angle markings, fixed to the frame of a gyroscope providing an artificial horizon 17, and a transparent circular plate 31 carrying a line 38. The plate 31 is rotated by a cable 41 relative to the instrument casing by the aileron control in the same sense as the ailerons rotate the aircraft. Thus, to achieve a desired angle of bank, the aileron controls are moved to tilt the line 38 to the corresponding bank angle on the ring 26, and as the instrument rotates (with the aircraft) and the ring remains upright, the aileron control is returned towards neutral to hold the line 38 stationary relative to the ring 26.
GB39773/65A 1965-09-17 1965-09-17 Control system for a vehicle, for example an aircraft Expired GB1076262A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB39773/65A GB1076262A (en) 1965-09-17 1965-09-17 Control system for a vehicle, for example an aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB39773/65A GB1076262A (en) 1965-09-17 1965-09-17 Control system for a vehicle, for example an aircraft

Publications (1)

Publication Number Publication Date
GB1076262A true GB1076262A (en) 1967-07-19

Family

ID=10411411

Family Applications (1)

Application Number Title Priority Date Filing Date
GB39773/65A Expired GB1076262A (en) 1965-09-17 1965-09-17 Control system for a vehicle, for example an aircraft

Country Status (1)

Country Link
GB (1) GB1076262A (en)

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