SE8402467L - WARNING SYSTEM FOR ATTENTION TO A PILOT ON A DANGEROUS FLIGHT PROFILE DURING AHEAD FLIGHT - Google Patents

WARNING SYSTEM FOR ATTENTION TO A PILOT ON A DANGEROUS FLIGHT PROFILE DURING AHEAD FLIGHT

Info

Publication number
SE8402467L
SE8402467L SE8402467A SE8402467A SE8402467L SE 8402467 L SE8402467 L SE 8402467L SE 8402467 A SE8402467 A SE 8402467A SE 8402467 A SE8402467 A SE 8402467A SE 8402467 L SE8402467 L SE 8402467L
Authority
SE
Sweden
Prior art keywords
aircraft
pilot
flight
attention
warning system
Prior art date
Application number
SE8402467A
Other languages
Unknown language ( )
Swedish (sv)
Other versions
SE8402467D0 (en
Inventor
N S Paterson
E E Vermilion
Original Assignee
Sundstrand Data Control
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 filed Critical Sundstrand Data Control
Publication of SE8402467D0 publication Critical patent/SE8402467D0/en
Publication of SE8402467L publication Critical patent/SE8402467L/en

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
    • G01P1/00—Details of instruments
    • G01P1/07—Indicating devices, e.g. for remote indication
    • G01P1/08—Arrangements of scales, pointers, lamps or acoustic indicators, e.g. in automobile speedometers
    • G01P1/10—Arrangements of scales, pointers, lamps or acoustic indicators, e.g. in automobile speedometers for indicating predetermined speeds

Abstract

A system that warns the pilot of an aircraft performing low level maneuvers of a dangerous flight profile monitors the altitude of the aircraft above ground, and provides a first specific warning to the pilot if the altitude of the aircraft drops below a predetermined minimum altitude above ground. The system further monitors the roll angle and descent rate of the aircraft to provide a second specific warning if the descent rate of the aircraft exceeds a predetermined rate determined by the roll angle of the aircraft if the aircraft is below a second predetermined altitude above ground. <IMAGE>
SE8402467A 1983-05-13 1984-05-08 WARNING SYSTEM FOR ATTENTION TO A PILOT ON A DANGEROUS FLIGHT PROFILE DURING AHEAD FLIGHT SE8402467L (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US49459083A 1983-05-13 1983-05-13

Publications (2)

Publication Number Publication Date
SE8402467D0 SE8402467D0 (en) 1984-05-08
SE8402467L true SE8402467L (en) 1984-11-14

Family

ID=23965099

Family Applications (1)

Application Number Title Priority Date Filing Date
SE8402467A SE8402467L (en) 1983-05-13 1984-05-08 WARNING SYSTEM FOR ATTENTION TO A PILOT ON A DANGEROUS FLIGHT PROFILE DURING AHEAD FLIGHT

Country Status (15)

Country Link
JP (1) JPS59216795A (en)
AU (2) AU548709B2 (en)
BE (1) BE899643A (en)
CA (1) CA1234417A (en)
CH (1) CH660156A5 (en)
DE (1) DE3417884A1 (en)
ES (2) ES532430A0 (en)
FI (1) FI74251C (en)
FR (1) FR2550334B1 (en)
GB (2) GB2139588B (en)
GR (1) GR82062B (en)
IL (1) IL71348A (en)
IT (1) IT1177721B (en)
NL (1) NL8401531A (en)
SE (1) SE8402467L (en)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5001476A (en) * 1983-05-13 1991-03-19 Sundstrand Data Control, Inc. Warning system for tactical aircraft
CA1243405A (en) * 1985-02-22 1988-10-18 Michael M. Grove Configuration responsive descent rate warning system for aircraft
CA1243119A (en) * 1985-02-22 1988-10-11 Michael M. Grove Aircraft terrain warning system with configuration modified warning and improved mode switching
DE3621052A1 (en) * 1986-06-24 1988-01-07 Aerodata Flugmesstechnik Gmbh Device for the automatic flight path guidance of aircraft along a guidance beam
CH671555A5 (en) * 1986-09-10 1989-09-15 Zermatt Air Ag
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
US5864307A (en) * 1996-02-19 1999-01-26 Gec Marconi Limited Aircraft terrain advisory system
FR2749676B1 (en) * 1996-06-11 1998-09-11 Sextant Avionique ALTITUDE MANAGEMENT METHOD AND SYSTEM FOR AERODYNE
DE102007048956B4 (en) * 2007-10-12 2019-02-14 Airbus Operations Gmbh Apparatus and method for providing a flight status signal
US8155804B2 (en) 2007-10-12 2012-04-10 Airbus Operations Gmbh Device and method for providing a flight status signal
US8086361B2 (en) * 2007-12-12 2011-12-27 Honeywell International Inc. Advisory system to aid pilot recovery from spatial disorientation during an excessive roll
EP2592381A1 (en) 2011-11-08 2013-05-15 EADS Construcciones Aeronauticas, S.A. Discrete signal consolidation device and method and aircraft with said device

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3946358A (en) * 1974-06-19 1976-03-23 Sundstrand Data Control, Inc. Aircraft ground proximity warning instrument
US3947808A (en) * 1975-01-13 1976-03-30 Sundstrand Data Control, Inc. Excessive descent rate warning system for aircraft
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
GB1567553A (en) * 1976-06-14 1980-05-14 Litton Industries Inc Digital ground proximity warning systems
US4319218A (en) * 1980-01-04 1982-03-09 Sundstrand Corporation Negative climb after take-off warning system with configuration warning means

Also Published As

Publication number Publication date
AU5506786A (en) 1986-08-14
NL8401531A (en) 1984-12-03
ES8506523A1 (en) 1985-08-01
IL71348A (en) 1989-09-10
GB2175264B (en) 1987-04-15
CA1234417A (en) 1988-03-22
FI74251B (en) 1987-09-30
AU2668784A (en) 1984-11-15
FR2550334B1 (en) 1988-04-15
GR82062B (en) 1984-12-13
GB2139588B (en) 1987-04-15
AU548709B2 (en) 1986-01-02
FR2550334A1 (en) 1985-02-08
GB8611002D0 (en) 1986-06-11
CH660156A5 (en) 1987-03-31
ES8607158A1 (en) 1986-05-16
FI841910A (en) 1984-11-14
IT8448181A0 (en) 1984-05-11
ES541246A0 (en) 1986-05-16
ES532430A0 (en) 1985-08-01
DE3417884C2 (en) 1990-04-19
IT1177721B (en) 1987-08-26
FI74251C (en) 1988-01-11
FI841910A0 (en) 1984-05-11
DE3417884A1 (en) 1984-12-13
BE899643A (en) 1984-11-12
GB8411768D0 (en) 1984-06-13
GB2139588A (en) 1984-11-14
GB2175264A (en) 1986-11-26
JPS59216795A (en) 1984-12-06
SE8402467D0 (en) 1984-05-08

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Effective date: 19901115