GB829740A - Aircraft pitch-attitude control apparatus - Google Patents

Aircraft pitch-attitude control apparatus

Info

Publication number
GB829740A
GB829740A GB20847/59A GB2084759A GB829740A GB 829740 A GB829740 A GB 829740A GB 20847/59 A GB20847/59 A GB 20847/59A GB 2084759 A GB2084759 A GB 2084759A GB 829740 A GB829740 A GB 829740A
Authority
GB
United Kingdom
Prior art keywords
signal dependent
deviation
aircraft
control apparatus
attitude control
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
GB20847/59A
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.)
Sperry Corp
Original Assignee
Sperry Rand 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 Sperry Rand Corp filed Critical Sperry Rand Corp
Publication of GB829740A publication Critical patent/GB829740A/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
    • G05D1/04—Control of altitude or depth
    • G05D1/06—Rate of change of altitude or depth
    • G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft
    • G05D1/0615—Rate of change of altitude or depth specially adapted for aircraft to counteract a perturbation, e.g. gust of wind
    • G05D1/0623—Rate of change of altitude or depth specially adapted for aircraft to counteract a perturbation, e.g. gust of wind by acting on the pitch

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)

Abstract

829,740. Automatic control systems for aircraft. SPERRY RAND CORPORATION. Feb. 15, 1957 [March 15, 1956], No. 20847/59. Divided out of 829,739. Drawings to Specification. Class 38 (4). The subject-matter of this Specification is identical with that in Specification 829,739, but the claims are directed to an aircraft automatic pilot in which a signal dependent on deviation of altitude, speed, or Mach number from a desired value is applied, together with a signal dependent on acceleration along the yaw axis, to an integrator, the output of which is combined with the signal dependent on altitude, speed, or Mach number deviation, and a signal dependent on deviation of pitch from a reference value, to control an elevator servomotor. Specification 612,804 also is referred to.
GB20847/59A 1956-03-15 1957-02-15 Aircraft pitch-attitude control apparatus Expired GB829740A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US829740XA 1956-03-15 1956-03-15

Publications (1)

Publication Number Publication Date
GB829740A true GB829740A (en) 1960-03-09

Family

ID=22174624

Family Applications (1)

Application Number Title Priority Date Filing Date
GB20847/59A Expired GB829740A (en) 1956-03-15 1957-02-15 Aircraft pitch-attitude control apparatus

Country Status (1)

Country Link
GB (1) GB829740A (en)

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