FR2474725A1 - Systeme et instrument d'avertissement de la proximite du sol pour un aeronef - Google Patents

Systeme et instrument d'avertissement de la proximite du sol pour un aeronef Download PDF

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Publication number
FR2474725A1
FR2474725A1 FR8026938A FR8026938A FR2474725A1 FR 2474725 A1 FR2474725 A1 FR 2474725A1 FR 8026938 A FR8026938 A FR 8026938A FR 8026938 A FR8026938 A FR 8026938A FR 2474725 A1 FR2474725 A1 FR 2474725A1
Authority
FR
France
Prior art keywords
aircraft
signal
warning
altitude
configuration
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.)
Granted
Application number
FR8026938A
Other languages
English (en)
French (fr)
Other versions
FR2474725B1 (US07576130-20090818-C00114.png
Inventor
Charles Donald Bateman
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 Data Control Inc
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 FR2474725A1 publication Critical patent/FR2474725A1/fr
Application granted granted Critical
Publication of FR2474725B1 publication Critical patent/FR2474725B1/fr
Granted 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
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P3/00—Measuring linear or angular speed; Measuring differences of linear or angular speeds
    • G01P3/62—Devices characterised by the determination or the variation of atmospheric pressure with height to measure the vertical components of speed
    • 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

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Emergency Alarm Devices (AREA)
  • Traffic Control Systems (AREA)
  • Navigation (AREA)
FR8026938A 1980-01-04 1980-12-18 Systeme et instrument d'avertissement de la proximite du sol pour un aeronef Granted FR2474725A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/109,580 US4319218A (en) 1980-01-04 1980-01-04 Negative climb after take-off warning system with configuration warning means

Publications (2)

Publication Number Publication Date
FR2474725A1 true FR2474725A1 (fr) 1981-07-31
FR2474725B1 FR2474725B1 (US07576130-20090818-C00114.png) 1984-10-19

Family

ID=22328427

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8026938A Granted FR2474725A1 (fr) 1980-01-04 1980-12-18 Systeme et instrument d'avertissement de la proximite du sol pour un aeronef

Country Status (15)

Country Link
US (1) US4319218A (US07576130-20090818-C00114.png)
JP (2) JPS56101300A (US07576130-20090818-C00114.png)
AU (1) AU521987B2 (US07576130-20090818-C00114.png)
CA (1) CA1157132A (US07576130-20090818-C00114.png)
CH (1) CH652495A5 (US07576130-20090818-C00114.png)
DE (1) DE3044955A1 (US07576130-20090818-C00114.png)
FI (1) FI69991C (US07576130-20090818-C00114.png)
FR (1) FR2474725A1 (US07576130-20090818-C00114.png)
GB (2) GB2066759B (US07576130-20090818-C00114.png)
GR (1) GR73608B (US07576130-20090818-C00114.png)
IL (1) IL61755A (US07576130-20090818-C00114.png)
IT (1) IT1142204B (US07576130-20090818-C00114.png)
NL (1) NL8007109A (US07576130-20090818-C00114.png)
NZ (1) NZ195804A (US07576130-20090818-C00114.png)
SE (1) SE452300B (US07576130-20090818-C00114.png)

Families Citing this family (57)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4431994A (en) * 1981-05-06 1984-02-14 The United States Of America As Represented By The Secretary Of The Air Force Combined radar/barometric altimeter
US4433323A (en) * 1982-02-04 1984-02-21 Sundstrand Data Control, Inc. Ground proximity warning system with time and altitude based mode switching
US4516124A (en) * 1982-07-22 1985-05-07 Harry D. Shannon Convertible amphibious aircraft wheel position warning system
US4567483A (en) * 1982-12-10 1986-01-28 Sundstrand Data Control, Inc. Position based ground proximity warning system for aircraft
US4916447A (en) * 1983-05-13 1990-04-10 Sundstrand Data Control, Inc. Warning system for aircraft landing with landing gear up
NZ207653A (en) * 1983-05-13 1987-11-27 Sundstrand Data Control Excessive descent rate warning system for aircraft
US4939513A (en) * 1983-05-13 1990-07-03 Sundstrand Data Control, Inc. System for alerting a pilot of a dangerous flight profile during low level maneuvering
CA1234417A (en) * 1983-05-13 1988-03-22 Noel S. Paterson System for alerting a pilot of a dangerous flight profile during low level maneuvering
US4951047A (en) * 1983-05-13 1990-08-21 Sunstrand Data Control, Inc. Negative climb after take-off warning system
US4639730A (en) * 1983-05-13 1987-01-27 Sundstrand Data Control, Inc. Excessive terrain closure warning system
US4551723A (en) * 1983-06-10 1985-11-05 Sundstrand Data Control, Inc. Excessive descent rate warning system for rotary wing aircraft
US4818992A (en) * 1983-06-10 1989-04-04 Sundstrand Data Control, Inc. Excessive altitude loss after take-off warning system for rotary wing aircraft
US5220322A (en) * 1984-07-18 1993-06-15 Sundstrand Corporation Ground proximity warning system for use with aircraft having egraded performance
IL77860A0 (en) * 1985-02-22 1986-09-30 Sundstrand Data Control Ground proximity warning system for aircraft
CA1243117A (en) * 1985-02-22 1988-10-11 Michael M. Grove Altitude loss after take-off warning system utilizing time and altitude
DE3621052A1 (de) * 1986-06-24 1988-01-07 Aerodata Flugmesstechnik Gmbh Vorrichtung zur automatischen flugbahnfuehrung von flugzeugen laengs eines leitstrahls
JPS63153124U (US07576130-20090818-C00114.png) * 1987-03-27 1988-10-07
US5047942A (en) * 1987-08-06 1991-09-10 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Airplane takeoff and landing performance monitoring system
US5519391A (en) * 1994-09-07 1996-05-21 Alliedsignal Inc. Improper flap position on take-off warning
US5666110A (en) * 1995-03-09 1997-09-09 Paterson; Noel S. Helicopter enhanced descent after take-off warning for GPWS
US6092009A (en) * 1995-07-31 2000-07-18 Alliedsignal Aircraft terrain information system
US6292721B1 (en) 1995-07-31 2001-09-18 Allied Signal Inc. Premature descent into terrain visual awareness enhancement to EGPWS
US6606034B1 (en) 1995-07-31 2003-08-12 Honeywell International Inc. Terrain awareness system
US6691004B2 (en) 1995-07-31 2004-02-10 Honeywell International, Inc. Method for determining a currently obtainable climb gradient of an aircraft
US5839080B1 (en) * 1995-07-31 2000-10-17 Allied Signal Inc Terrain awareness system
US6138060A (en) * 1995-07-31 2000-10-24 Alliedsignal Inc. Terrain awareness system
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
US5781126A (en) * 1996-07-29 1998-07-14 Alliedsignal Inc. Ground proximity warning system and methods for rotary wing aircraft
US6043759A (en) * 1996-07-29 2000-03-28 Alliedsignal Air-ground logic system and method for rotary wing aircraft
EP0988630A4 (en) * 1997-03-20 2006-01-18 Innovative Solutions & Support AIR DATA MEASUREMENT WITH LINEARIZATION CIRCUIT FOR THE PRESSURE SENSOR OUTPUT SIGNAL
US6643580B1 (en) 1998-10-16 2003-11-04 Universal Avionics Systems Corporation Flight plan intent alert system and method
EP1151429B1 (en) 1999-02-01 2004-04-07 Honeywell International Inc. System for generating altitudes above a selected runway
WO2000045126A1 (en) 1999-02-01 2000-08-03 Honeywell International Inc. Ground proximity warning system
US6484071B1 (en) 1999-02-01 2002-11-19 Honeywell International, Inc. Ground proximity warning system, method and computer program product for controllably altering the base width of an alert envelope
WO2000054120A2 (en) 1999-02-01 2000-09-14 Honeywell International Inc. Methods, apparatus and computer program products for determining a corrected distance between an aircraft and a selected runway
EP1155285B1 (en) 1999-02-01 2004-07-07 Honeywell International Inc. Apparatus, method, and computer program product for generating terrain clearance floor envelopes about a selected runway
US6785594B1 (en) 1999-03-25 2004-08-31 Honeywell International Inc. Ground proximity warning system and method having a reduced set of input parameters
US6734808B1 (en) 1999-10-05 2004-05-11 Honeywell International Inc. Method, apparatus and computer program products for alerting submersible vessels to hazardous conditions
US6469664B1 (en) 1999-10-05 2002-10-22 Honeywell International Inc. Method, apparatus, and computer program products for alerting surface vessels to hazardous conditions
US6833797B2 (en) 2000-05-26 2004-12-21 Honeywell International Inc. Method, apparatus and computer program product for displaying terrain in rotary wing aircraft
US6583733B2 (en) 2000-05-26 2003-06-24 Honeywell International Inc. Apparatus, method and computer program product for helicopter ground proximity warning system
EP1317652B1 (en) 2000-09-14 2010-11-10 Honeywell International Inc. Method, apparatus and computer program product for helicopter tail strike warning
RU2282157C2 (ru) * 2001-07-17 2006-08-20 Хонейвелл Интернэшнл, Инк. Устройство предупреждения об опасном угле тангажа для улучшенной системы предупреждения опасного сближения с землей (успос)
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
JP5499665B2 (ja) * 2009-12-01 2014-05-21 株式会社アドヴィックス 車両用制御装置
US9051061B2 (en) * 2012-12-14 2015-06-09 Safe Flight Instrument Corporation Systems and methods for safely landing an aircraft
US9828113B2 (en) 2013-11-05 2017-11-28 Safe Flight Instrument Corporation Tailstrike warning system
US9546003B2 (en) 2014-03-14 2017-01-17 Safe Flight Instrument Corporation Deflare pitch command
US9346552B2 (en) 2014-04-11 2016-05-24 Safe Flight Instrument Corporation Autothrottle retard control
US20150321748A1 (en) * 2014-05-08 2015-11-12 Honeywell International Inc. Speed brake alerting system and method
US20170008639A1 (en) 2015-07-08 2017-01-12 Safe Flight Instrument Corporation Aircraft turbulence detection
EP3127818A1 (en) * 2015-08-06 2017-02-08 Mitsubishi Aircraft Corporation Computer system for determining approach of aircraft and aircraft
JP6683444B2 (ja) 2015-08-06 2020-04-22 三菱航空機株式会社 航空機のアプローチを判定するコンピュータシステムおよび航空機
GB2587205A (en) * 2019-09-17 2021-03-24 Airbus Operations Ltd Aircraft system
CN112455662B (zh) * 2020-09-18 2024-02-02 中电科芜湖通用航空产业技术研究院有限公司 飞机起落架警告发起及消除电路和方法

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2299682A1 (fr) * 1975-01-30 1976-08-27 Plessey Handel Investment Ag Installation d'avertissement, notamment de la proximite du sol, pour engins aeriens
FR2306430A1 (fr) * 1975-04-02 1976-10-29 Sundstrand Data Control Dispositif d'alarme d'approche du sol avec mesure d'augmentation d'altitude
FR2309939A1 (fr) * 1974-06-19 1976-11-26 Sundstrand Data Control Appareil d'alarme de proximite du sol
FR2359425A1 (fr) * 1976-07-19 1978-02-17 Sundstrand Data Control Circuit d'avertissement de vitesse excessive de descente d'un aeronef
FR2359396A1 (fr) * 1976-07-19 1978-02-17 Sundstrand Data Control Circuit d'avertissement de distance au sol pour aeronef

Family Cites Families (4)

* 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
US3936796A (en) * 1974-06-19 1976-02-03 Sundstrand Data Control, Inc. Aircraft ground proximity warning instrument
US3947810A (en) * 1975-01-13 1976-03-30 Sundstrand Data Control, Inc. Negative climb rate after take-off warning system with predetermined loss of altitude inhibit
US3925751A (en) * 1975-04-02 1975-12-09 Sundstrand Data Control Glide slope warning system with a variable warning rate

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2309939A1 (fr) * 1974-06-19 1976-11-26 Sundstrand Data Control Appareil d'alarme de proximite du sol
FR2299682A1 (fr) * 1975-01-30 1976-08-27 Plessey Handel Investment Ag Installation d'avertissement, notamment de la proximite du sol, pour engins aeriens
FR2306430A1 (fr) * 1975-04-02 1976-10-29 Sundstrand Data Control Dispositif d'alarme d'approche du sol avec mesure d'augmentation d'altitude
FR2359425A1 (fr) * 1976-07-19 1978-02-17 Sundstrand Data Control Circuit d'avertissement de vitesse excessive de descente d'un aeronef
FR2359396A1 (fr) * 1976-07-19 1978-02-17 Sundstrand Data Control Circuit d'avertissement de distance au sol pour aeronef

Also Published As

Publication number Publication date
AU6515980A (en) 1981-07-09
IL61755A (en) 1987-10-30
GB8319496D0 (en) 1983-08-17
FI810003L (fi) 1981-07-05
SE8008867L (sv) 1981-07-05
FR2474725B1 (US07576130-20090818-C00114.png) 1984-10-19
IT1142204B (it) 1986-10-08
JPS628127B2 (US07576130-20090818-C00114.png) 1987-02-20
FI69991C (fi) 1986-09-12
DE3044955A1 (de) 1981-07-09
IT8147504A0 (it) 1981-01-02
GB2066759A (en) 1981-07-15
DE3044955C2 (US07576130-20090818-C00114.png) 1988-02-25
SE452300B (sv) 1987-11-23
NZ195804A (en) 1984-12-14
GR73608B (US07576130-20090818-C00114.png) 1984-03-26
GB2126184B (en) 1984-08-15
GB2126184A (en) 1984-03-21
US4319218A (en) 1982-03-09
AU521987B2 (en) 1982-05-13
JPS56101300A (en) 1981-08-13
CH652495A5 (de) 1985-11-15
JPS628724B2 (US07576130-20090818-C00114.png) 1987-02-24
GB2066759B (en) 1984-04-04
CA1157132A (en) 1983-11-15
JPS6121600A (ja) 1986-01-30
NL8007109A (nl) 1981-08-03
FI69991B (fi) 1986-01-31

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