DE3685790T2 - Flugzeugterrainannaeherungswarnsystem mit auf die abstieggeschwindigkeit basierten huellenaenderung. - Google Patents

Flugzeugterrainannaeherungswarnsystem mit auf die abstieggeschwindigkeit basierten huellenaenderung.

Info

Publication number
DE3685790T2
DE3685790T2 DE8686902091T DE3685790T DE3685790T2 DE 3685790 T2 DE3685790 T2 DE 3685790T2 DE 8686902091 T DE8686902091 T DE 8686902091T DE 3685790 T DE3685790 T DE 3685790T DE 3685790 T2 DE3685790 T2 DE 3685790T2
Authority
DE
Germany
Prior art keywords
airplane
climate
warning system
change based
descent speed
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 - Fee Related
Application number
DE8686902091T
Other languages
English (en)
Other versions
DE3685790D1 (de
Inventor
M Grove
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.)
Sundstrand Corp
Original Assignee
Sundstrand Data Control Inc
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 Sundstrand Data Control Inc filed Critical Sundstrand Data Control Inc
Publication of DE3685790D1 publication Critical patent/DE3685790D1/de
Application granted granted Critical
Publication of DE3685790T2 publication Critical patent/DE3685790T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C5/00—Measuring height; Measuring distances transverse to line of sight; Levelling between separated points; Surveyors' levels
    • G01C5/005—Measuring height; Measuring distances transverse to line of sight; Levelling between separated points; Surveyors' levels altimeters for aircraft

Landscapes

  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Emergency Alarm Devices (AREA)
DE8686902091T 1985-02-22 1986-02-21 Flugzeugterrainannaeherungswarnsystem mit auf die abstieggeschwindigkeit basierten huellenaenderung. Expired - Fee Related DE3685790T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US70436585A 1985-02-22 1985-02-22
PCT/US1986/000384 WO1986005023A1 (en) 1985-02-22 1986-02-21 Aircraft terrain closure warning system with descent rate based envelope modification

Publications (2)

Publication Number Publication Date
DE3685790D1 DE3685790D1 (de) 1992-07-30
DE3685790T2 true DE3685790T2 (de) 1993-02-11

Family

ID=24829167

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8686902091T Expired - Fee Related DE3685790T2 (de) 1985-02-22 1986-02-21 Flugzeugterrainannaeherungswarnsystem mit auf die abstieggeschwindigkeit basierten huellenaenderung.

Country Status (7)

Country Link
US (1) US4792799A (de)
EP (1) EP0217852B1 (de)
JP (1) JPS62500264A (de)
CA (1) CA1243118A (de)
DE (1) DE3685790T2 (de)
FI (1) FI864239A (de)
WO (1) WO1986005023A1 (de)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5202684A (en) * 1985-10-17 1993-04-13 Toyo Communication Equipment Co., Ltd. System of an aircraft collision avoidance system for suppressing useless alarms
US4916448A (en) * 1988-02-26 1990-04-10 The United States Of America As Represented By The Secretary Of The Air Force Low altitude warning system for aircraft
US5136512A (en) * 1988-06-26 1992-08-04 Cubic Defense Systems, Inc. Ground collision avoidance system
US5349347A (en) * 1993-03-29 1994-09-20 Alliedsignal Inc. Method and apparatus for correcting dynamically induced errors in static pressure, airspeed and airspeed rate
US5428354A (en) * 1993-11-05 1995-06-27 Alliedsignal Inc. Ground proximity warning system for non-retractable landing gear aircraft
SE9401847L (sv) * 1994-05-30 1995-05-22 Saab Scania Ab Metod och anordning för att utföra faskompensering i ett fordons styrsystem
FR2728374A1 (fr) * 1994-12-15 1996-06-21 Aerospatiale Procede et dispositif pour fournir une information, alerte ou alarme pour un aeronef a proximite du sol
US5745053A (en) * 1995-12-08 1998-04-28 Fleming, Iii; Hoyt A. Landing gear warning apparatus and method for pilots approaching a runway with retracted landing gear
US5828332A (en) * 1996-03-11 1998-10-27 Imaging Accessories, Inc. Automatic horizontal and vertical scanning radar with terrain display
US5781146A (en) * 1996-03-11 1998-07-14 Imaging Accessories, Inc. Automatic horizontal and vertical scanning radar with terrain display
US6745115B1 (en) 2003-01-07 2004-06-01 Garmin Ltd. System, method and apparatus for searching geographic area using prioritized spacial order
US7386373B1 (en) * 2003-01-07 2008-06-10 Garmin International, Inc. System, method and apparatus for searching geographic area using prioritized spatial order
US7382287B1 (en) 2003-06-03 2008-06-03 Garmin International, Inc Avionics system, method and apparatus for selecting a runway
US6980892B1 (en) 2003-11-18 2005-12-27 Garmin International, Inc. Avionics system and method for providing altitude alerts during final landing approach
US8624757B2 (en) * 2011-06-27 2014-01-07 General Electric Company Method for visually indicating an advisory from the traffic collision avoidance system on a flight display
FR3036497B1 (fr) * 2015-05-19 2017-06-16 Airbus Operations Sas Procede et systeme de gestion de donnees d'un radioaltimetre d'aeronef.
US9751636B2 (en) 2015-12-15 2017-09-05 International Business Machines Corporation Dynamic detection of landing gear deployment

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3715718A (en) * 1970-08-11 1973-02-06 Sundstrand Data Control Ground proximity warning system utilizing radio and barometric altimeter combination
US3946358A (en) * 1974-06-19 1976-03-23 Sundstrand Data Control, Inc. Aircraft ground proximity warning instrument
US3958218A (en) * 1974-10-03 1976-05-18 Sundstrand Data Control, Inc. Aircraft ground proximity warning system with speed compensation
US3944968A (en) * 1974-11-01 1976-03-16 Sundstrand Data Control, Inc. Aircraft ground proximity warning system having speed versus altitude compensation
US3934221A (en) * 1975-03-06 1976-01-20 Sundstrand Data Control, Inc. Terrain closure warning system with altitude rate signal conditioning
US3958219A (en) * 1975-03-06 1976-05-18 Sundstrand Data Control, Inc. Terrain closure warning system with altitude rate signal conditioning
US3934222A (en) * 1975-04-02 1976-01-20 Sundstrand Data Control, Inc. Terrain closure warning system with climb inhibit and altitude gain measurement
US4016565A (en) * 1975-09-15 1977-04-05 Rockwell International Corporation Aircraft ground closure rate filtering method and means
US4060793A (en) * 1976-07-19 1977-11-29 Sundstrand Data Control, Inc. Excessive sink rate warning system for aircraft
US4215334A (en) * 1978-02-09 1980-07-29 Sundstrand Data Control, Inc. Aircraft excessive descent rate warning system
US4495483A (en) * 1981-04-30 1985-01-22 Sundstrand Corporation Ground proximity warning system with time based mode switching
US4567483A (en) * 1982-12-10 1986-01-28 Sundstrand Data Control, Inc. Position based ground proximity warning system for aircraft
US4639730A (en) * 1983-05-13 1987-01-27 Sundstrand Data Control, Inc. Excessive terrain closure warning system
CA1241082A (en) * 1983-05-13 1988-08-23 Everette E. Vermilion Warning system for tactical aircraft
US4551723A (en) * 1983-06-10 1985-11-05 Sundstrand Data Control, Inc. Excessive descent rate warning system for rotary wing aircraft

Also Published As

Publication number Publication date
DE3685790D1 (de) 1992-07-30
FI864239A0 (fi) 1986-10-20
FI864239A (fi) 1986-10-20
EP0217852A4 (de) 1987-07-06
JPS62500264A (ja) 1987-01-29
WO1986005023A1 (en) 1986-08-28
CA1243118A (en) 1988-10-11
EP0217852A1 (de) 1987-04-15
EP0217852B1 (de) 1992-06-24
US4792799A (en) 1988-12-20

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: SUNDSTRAND CORP. (N.D.GES.D.STAATES DELAWARE), ROC

8339 Ceased/non-payment of the annual fee