FR1564107A - - Google Patents

Info

Publication number
FR1564107A
FR1564107A FR1564107DA FR1564107A FR 1564107 A FR1564107 A FR 1564107A FR 1564107D A FR1564107D A FR 1564107DA FR 1564107 A FR1564107 A FR 1564107A
Authority
FR
France
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
Other languages
French (fr)
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 filed Critical
Application granted granted Critical
Publication of FR1564107A publication Critical patent/FR1564107A/fr
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F1/00—Ground or aircraft-carrier-deck installations
    • B64F1/18—Visual or acoustic landing aids
    • B64F1/20—Arrangement of optical beacons
    • 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
    • G05D1/0653—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing
    • G05D1/0676—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for landing
    • G05D1/0684—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for landing on a moving platform, e.g. aircraft carrier
    • 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
    • G05D1/0858—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft specially adapted for vertical take-off of aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Acoustics & Sound (AREA)
  • Mechanical Engineering (AREA)
FR1564107D 1967-03-22 1968-03-20 Expired FR1564107A (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US62524367A 1967-03-22 1967-03-22
US62919167A 1967-04-07 1967-04-07
US66031867A 1967-08-14 1967-08-14

Publications (1)

Publication Number Publication Date
FR1564107A true FR1564107A (en) 1969-04-18

Family

ID=27417371

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1564107D Expired FR1564107A (en) 1967-03-22 1968-03-20

Country Status (1)

Country Link
FR (1) FR1564107A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2631921A1 (en) * 1988-05-31 1989-12-01 Briatte Louis Michel AERONAUTICAL OPTICAL GUIDANCE ASSEMBLY

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2631921A1 (en) * 1988-05-31 1989-12-01 Briatte Louis Michel AERONAUTICAL OPTICAL GUIDANCE ASSEMBLY
EP0345141A1 (en) * 1988-05-31 1989-12-06 Societe Financiere Pour L'electronique Aeronautical guidance system
US5119090A (en) * 1988-05-31 1992-06-02 Britec Aeronautical optical guidance system

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Legal Events

Date Code Title Description
ST Notification of lapse