SE318121B - - Google Patents

Info

Publication number
SE318121B
SE318121B SE12801/63A SE1280163A SE318121B SE 318121 B SE318121 B SE 318121B SE 12801/63 A SE12801/63 A SE 12801/63A SE 1280163 A SE1280163 A SE 1280163A SE 318121 B SE318121 B SE 318121B
Authority
SE
Sweden
Application number
SE12801/63A
Inventor
R Bishop
E Kendall
R Palmer
Original Assignee
Smith & Sons Ltd S
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 Smith & Sons Ltd S filed Critical Smith & Sons Ltd S
Publication of SE318121B publication Critical patent/SE318121B/xx

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
    • G05D1/04Control of altitude or depth
    • G05D1/06Rate of change of altitude or depth
    • G05D1/0607Rate of change of altitude or depth specially adapted for aircraft
    • G05D1/0653Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing
    • G05D1/0661Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for take-off

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)
  • Navigation (AREA)
SE12801/63A 1962-11-20 1963-11-20 SE318121B (en:Method)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB43762/62A GB1032466A (en) 1962-11-20 1962-11-20 Improvements in or relating to aircraft instruments

Publications (1)

Publication Number Publication Date
SE318121B true SE318121B (en:Method) 1969-12-01

Family

ID=10430208

Family Applications (1)

Application Number Title Priority Date Filing Date
SE12801/63A SE318121B (en:Method) 1962-11-20 1963-11-20

Country Status (6)

Country Link
US (1) US3309923A (en:Method)
JP (1) JPS536437B1 (en:Method)
CH (1) CH411588A (en:Method)
DE (1) DE1292007B (en:Method)
GB (1) GB1032466A (en:Method)
SE (1) SE318121B (en:Method)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1071882A (en) * 1964-05-19 1967-06-14 Sperry Gyroscope Co Ltd Take-off director
GB1161408A (en) * 1965-11-03 1969-08-13 Sperry Rand Ltd Take-Off Director
GB2034892B (en) * 1978-11-14 1983-02-16 Ferranti Ltd Monitoring acceleration of aircraft moving along the ground
GB9003653D0 (en) * 1990-02-17 1990-04-11 Smiths Industries Plc Aircraft performance monitoring
GB9508659D0 (en) * 1995-04-28 1995-06-14 Smiths Industries Plc Aircraft instruments
CN113154193A (zh) * 2021-02-23 2021-07-23 韩玉坤 一种便于调节的野外便携式测绘设备

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2841345A (en) * 1952-01-15 1958-07-01 Sperry Rand Corp Glide path system with flare out
US3031662A (en) * 1956-07-02 1962-04-24 North American Aviation Inc Automatic landing system
DE1111515B (de) * 1956-10-01 1961-07-20 Sperry Rand Corp Sicherheitseinrichtung in Luftfahrzeugen zur UEberwachung des Startanlaufes
US3025494A (en) * 1958-01-24 1962-03-13 Kollsman Instr Corp Take-off indicator for aircraft
GB866228A (en) * 1958-07-18 1961-04-26 Kelvin & Hughes Ltd Improvements in and relating to take-off indicators for aircraft
GB874196A (en) * 1958-09-04 1961-08-02 Bendix Corp Aircraft take-off monitoring
GB909231A (en) * 1958-09-07 1962-10-31 Westinghouse Brake & Signal Improvements in or relating to apparatus suitable for automatically controlling a retarder in a hump yard
GB909175A (en) * 1960-05-20 1962-10-24 Smith & Sons Ltd S Improvements in and relating to aircraft ground run predictors
US3200642A (en) * 1962-06-25 1965-08-17 Charles A Neuendorf Maximum performance take-off director

Also Published As

Publication number Publication date
CH411588A (fr) 1966-04-15
DE1292007B (de) 1969-04-03
JPS536437B1 (en:Method) 1978-03-08
GB1032466A (en) 1966-06-08
US3309923A (en) 1967-03-21

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