ITTO921021A0 - TAKE-OFF AND LANDING SYSTEM - Google Patents

TAKE-OFF AND LANDING SYSTEM

Info

Publication number
ITTO921021A0
ITTO921021A0 IT92TO1021A ITTO921021A ITTO921021A0 IT TO921021 A0 ITTO921021 A0 IT TO921021A0 IT 92TO1021 A IT92TO1021 A IT 92TO1021A IT TO921021 A ITTO921021 A IT TO921021A IT TO921021 A0 ITTO921021 A0 IT TO921021A0
Authority
IT
Italy
Prior art keywords
take
landing system
landing
Prior art date
Application number
IT92TO1021A
Other languages
Italian (it)
Inventor
Wolfgang Alles
Hans-Peter Engelbert
Herbert Friedl
Klaus Kumpel
Michael Weidel
Original Assignee
Dornier Gmbh
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 Dornier Gmbh filed Critical Dornier Gmbh
Publication of ITTO921021A0 publication Critical patent/ITTO921021A0/en
Publication of ITTO921021A1 publication Critical patent/ITTO921021A1/en

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
    • G05D1/0653—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing
    • G05D1/0661—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for take-off
    • G05D1/0669—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for take-off specially adapted for vertical take-off
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters

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)
IT92TO001021A 1991-12-19 1992-12-18 TAKE-OFF AND LANDING SYSTEM ITTO921021A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE4142037A DE4142037A1 (en) 1991-12-19 1991-12-19 STARTING AND LANDING SYSTEM

Publications (2)

Publication Number Publication Date
ITTO921021A0 true ITTO921021A0 (en) 1992-12-18
ITTO921021A1 ITTO921021A1 (en) 1993-06-21

Family

ID=6447539

Family Applications (1)

Application Number Title Priority Date Filing Date
IT92TO001021A ITTO921021A1 (en) 1991-12-19 1992-12-18 TAKE-OFF AND LANDING SYSTEM

Country Status (5)

Country Link
CA (1) CA2085566A1 (en)
DE (1) DE4142037A1 (en)
FR (1) FR2686311A1 (en)
GB (1) GB2262626A (en)
IT (1) ITTO921021A1 (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6527225B1 (en) * 2002-04-30 2003-03-04 Sikorsky Aircraft Corporation Method for performing an automated category a takeoff
DE102007050246B4 (en) * 2007-10-20 2011-07-28 Diehl BGT Defence GmbH & Co. KG, 88662 Method and device for independent landing of a rotary wing aircraft
DE102008022838B4 (en) * 2008-05-08 2011-06-30 Deutsches Zentrum für Luft- und Raumfahrt e.V., 51147 Land auxiliary device
DE102008064712B4 (en) * 2008-05-08 2013-02-28 Deutsches Zentrum für Luft- und Raumfahrt e.V. Landing aid device for helicopter, has sensor unit with sensors for detecting relative position between landing platform and helicopter, where sensors are arranged for detecting relative velocity of landing platform against helicopter
DE102010051561A1 (en) * 2010-11-18 2012-05-24 Rheinmetall Defence Electronics Gmbh Automated landing of unmanned aerial vehicles
CN105222652A (en) * 2015-09-22 2016-01-06 长沙职业技术学院 The directional positioner of display shell, display shell and display shell direction and location method

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1293351A (en) * 1961-06-20 1962-05-11 electro-brake for aircraft landing
US4025193A (en) * 1974-02-11 1977-05-24 The Boeing Company Apparatus suitable for use in orienting aircraft in-flight for refueling or other purposes
GB2155736A (en) * 1984-03-08 1985-09-25 Smiths Industries Plc Aircraft position determination
FR2636303B1 (en) * 1988-09-14 1992-05-07 Telecommunications Sa ASSISTANCE SYSTEM FOR THE DECKING OF AIRCRAFT HAVING A STATIONARY FLIGHT ON A SHIP PLATFORM
IL88263A (en) * 1988-11-02 1993-03-15 Electro Optics Ind Ltd Navigation system
GB8922485D0 (en) * 1989-10-05 1989-11-22 Fairey Hydraulics Securing device
US5195039A (en) * 1990-05-03 1993-03-16 United Technologies Corporation Hover position hold system for rotary winged aircraft

Also Published As

Publication number Publication date
GB9224374D0 (en) 1993-01-13
DE4142037A1 (en) 1993-06-24
FR2686311A1 (en) 1993-07-23
ITTO921021A1 (en) 1993-06-21
GB2262626A (en) 1993-06-23
CA2085566A1 (en) 1993-06-20

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Legal Events

Date Code Title Description
0003 Withdrawn