WO2001090694A3 - Apparatus, method and computer program product for helicopter ground proximity warning system - Google Patents

Apparatus, method and computer program product for helicopter ground proximity warning system Download PDF

Info

Publication number
WO2001090694A3
WO2001090694A3 PCT/US2001/017228 US0117228W WO0190694A3 WO 2001090694 A3 WO2001090694 A3 WO 2001090694A3 US 0117228 W US0117228 W US 0117228W WO 0190694 A3 WO0190694 A3 WO 0190694A3
Authority
WO
WIPO (PCT)
Prior art keywords
computer program
program product
warning system
proximity warning
ground proximity
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.)
Ceased
Application number
PCT/US2001/017228
Other languages
French (fr)
Other versions
WO2001090694A2 (en
Inventor
Yasuo Ishihara
Kevin Conner
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.)
Honeywell International Inc
Original Assignee
Honeywell International 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 Honeywell International Inc filed Critical Honeywell International Inc
Priority to EP01958827A priority Critical patent/EP1290407B1/en
Priority to DE60138017T priority patent/DE60138017D1/en
Publication of WO2001090694A2 publication Critical patent/WO2001090694A2/en
Publication of WO2001090694A3 publication Critical patent/WO2001090694A3/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D45/04—Landing aids; Safety measures to prevent collision with earth's surface
    • 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
    • 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
    • G05D1/0646—Rate of change of altitude or depth specially adapted for aircraft to follow the profile of undulating ground
    • 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)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Traffic Control Systems (AREA)
  • Navigation (AREA)
  • Emergency Alarm Devices (AREA)
  • Alarm Systems (AREA)
  • Nozzles (AREA)
  • Toys (AREA)

Abstract

An apparatus, method and computer program product has a first terrain awareness mode and a second terrain awareness mode selectable by the pilot.
PCT/US2001/017228 2000-05-26 2001-05-25 Apparatus, method and computer program product for helicopter ground proximity warning system Ceased WO2001090694A2 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
EP01958827A EP1290407B1 (en) 2000-05-26 2001-05-25 Apparatus, method and computer program product for helicopter ground proximity warning system
DE60138017T DE60138017D1 (en) 2000-05-26 2001-05-25 Device, method and computer program product for a helicopter ground proximity warning system

Applications Claiming Priority (6)

Application Number Priority Date Filing Date Title
US20751500P 2000-05-26 2000-05-26
US20799800P 2000-05-26 2000-05-26
US20774000P 2000-05-26 2000-05-26
US60/207,515 2000-05-26
US60/207,998 2000-05-26
US60/207,740 2000-05-26

Publications (2)

Publication Number Publication Date
WO2001090694A2 WO2001090694A2 (en) 2001-11-29
WO2001090694A3 true WO2001090694A3 (en) 2002-04-18

Family

ID=27395072

Family Applications (3)

Application Number Title Priority Date Filing Date
PCT/US2001/017105 Ceased WO2001090693A2 (en) 2000-05-26 2001-05-25 Apparatus, method and computer program product for helicopter enhanced ground proximity warning system
PCT/US2001/017179 Ceased WO2001092823A2 (en) 2000-05-26 2001-05-25 Method, apparatus and computer program product for displaying terrain in rotary wing aircraft
PCT/US2001/017228 Ceased WO2001090694A2 (en) 2000-05-26 2001-05-25 Apparatus, method and computer program product for helicopter ground proximity warning system

Family Applications Before (2)

Application Number Title Priority Date Filing Date
PCT/US2001/017105 Ceased WO2001090693A2 (en) 2000-05-26 2001-05-25 Apparatus, method and computer program product for helicopter enhanced ground proximity warning system
PCT/US2001/017179 Ceased WO2001092823A2 (en) 2000-05-26 2001-05-25 Method, apparatus and computer program product for displaying terrain in rotary wing aircraft

Country Status (5)

Country Link
EP (3) EP1290407B1 (en)
JP (1) JP2003534987A (en)
AT (3) ATE426144T1 (en)
DE (3) DE60127250T2 (en)
WO (3) WO2001090693A2 (en)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8078344B2 (en) 2005-04-21 2011-12-13 Honeywell International Inc. System and method for displaying the protected airspace associated with a circle-to-land maneuver
FR2897839B1 (en) * 2006-02-27 2009-01-23 Airbus France Sas METHOD AND DEVICE FOR AUTOMATICALLY ADJUSTING AN IMAGE OF AN AIRCRAFT NAVIGATION SCREEN
US8098176B2 (en) * 2010-05-07 2012-01-17 Honeywell International Inc. Systems and methods for adjusting landing gear alert envelope for offshore platforms and building-top landings
FR2999156B1 (en) * 2012-12-12 2015-01-16 Thales Sa METHOD OF SECURING AN AIRCRAFT
CN103354041B (en) * 2013-06-25 2015-12-09 上海交通大学 A kind of civil aircraft terrain perception and warning system pattern four alarm envelope curve generation method
US9685091B2 (en) * 2013-08-30 2017-06-20 Insitu, Inc. Aerial vehicle awareness display
US9511880B2 (en) 2015-03-31 2016-12-06 Honeywell International Inc. Flight deck display systems and methods for generating vertical speed alerts during steep approaches of rotary wing aircraft
WO2017173416A1 (en) * 2016-03-31 2017-10-05 Netjets Inc. Aviation sector special departure procedure systems and methods
FR3063715B1 (en) 2017-03-09 2019-04-12 Dassault Aviation AIRCRAFT FLOOR PROXIMITY WARNING SYSTEM, AVIONICS AND ASSOCIATED METHOD
CN109903590B (en) * 2017-12-11 2023-04-07 上海航空电器有限公司 Terrain envelope-based aircraft automatic maneuver evasion method
FR3090978B1 (en) * 2018-12-19 2020-12-04 Airbus Helicopters method of detecting the proximity of a lateral arrangement of an aircraft with the ground and aircraft
US11908335B2 (en) 2022-07-13 2024-02-20 Honeywell International Inc. System and method for suggesting switching operational modes of a ground proximity warning system
US12434855B2 (en) 2022-08-12 2025-10-07 Subaru Corporation Aircraft

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6043759A (en) * 1996-07-29 2000-03-28 Alliedsignal Air-ground logic system and method for rotary wing aircraft

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4980684A (en) * 1983-06-10 1990-12-25 Sundstrand Data Controls, Inc. Warning system for tactical rotary wing aircraft
US5839080B1 (en) * 1995-07-31 2000-10-17 Allied Signal Inc Terrain awareness system
DE19831452C1 (en) * 1998-07-14 2000-03-09 Eurocopter Deutschland Procedures to support flight guidance

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6043759A (en) * 1996-07-29 2000-03-28 Alliedsignal Air-ground logic system and method for rotary wing aircraft

Also Published As

Publication number Publication date
WO2001090693A3 (en) 2002-04-18
DE60138015D1 (en) 2009-04-30
EP1290407B1 (en) 2009-03-18
ATE426144T1 (en) 2009-04-15
ATE426145T1 (en) 2009-04-15
WO2001090693A2 (en) 2001-11-29
WO2001092823A3 (en) 2002-05-23
EP1285227B1 (en) 2007-03-14
DE60127250T2 (en) 2007-12-06
EP1290407A2 (en) 2003-03-12
DE60127250D1 (en) 2007-04-26
WO2001090694A2 (en) 2001-11-29
ATE356972T1 (en) 2007-04-15
JP2003534987A (en) 2003-11-25
DE60138017D1 (en) 2009-04-30
EP1285227A2 (en) 2003-02-26
WO2001092823A2 (en) 2001-12-06
EP1285228A2 (en) 2003-02-26
EP1285228B1 (en) 2009-03-18

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