DE60016748D1 - Verfahren und vorrichtung zur bestimmung der vertikalgeschwindigkeit eines flugzeugs - Google Patents

Verfahren und vorrichtung zur bestimmung der vertikalgeschwindigkeit eines flugzeugs

Info

Publication number
DE60016748D1
DE60016748D1 DE60016748T DE60016748T DE60016748D1 DE 60016748 D1 DE60016748 D1 DE 60016748D1 DE 60016748 T DE60016748 T DE 60016748T DE 60016748 T DE60016748 T DE 60016748T DE 60016748 D1 DE60016748 D1 DE 60016748D1
Authority
DE
Germany
Prior art keywords
vertical
aircraft
vertical velocity
velocities
velocity
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 - Lifetime
Application number
DE60016748T
Other languages
English (en)
Other versions
DE60016748T2 (de
Inventor
C Johnson
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
Application granted granted Critical
Publication of DE60016748D1 publication Critical patent/DE60016748D1/de
Publication of DE60016748T2 publication Critical patent/DE60016748T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • 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
    • G01P3/42—Devices characterised by the use of electric or magnetic means
    • G01P3/50—Devices characterised by the use of electric or magnetic means for measuring linear speed
    • 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
    • G01P13/00—Indicating or recording presence, absence, or direction, of movement
    • G01P13/02—Indicating direction only, e.g. by weather vane
    • G01P13/025—Indicating direction only, e.g. by weather vane indicating air data, i.e. flight variables of an aircraft, e.g. angle of attack, side slip, shear, yaw
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P21/00—Testing or calibrating of apparatus or devices covered by the preceding groups
    • G01P21/02—Testing or calibrating of apparatus or devices covered by the preceding groups of speedometers
    • G01P21/025—Testing or calibrating of apparatus or devices covered by the preceding groups of speedometers for measuring speed of fluids; for measuring speed of bodies relative to fluids
    • 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
    • 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
    • G01P3/64—Devices characterised by the determination of the time taken to traverse a fixed distance
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
    • G01S19/01—Satellite radio beacon positioning systems transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
    • G01S19/13—Receivers
    • G01S19/14—Receivers specially adapted for specific applications
    • G01S19/15—Aircraft landing systems
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
    • G01S19/38—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system
    • G01S19/39—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system the satellite radio beacon positioning system transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
    • G01S19/42—Determining position
    • G01S19/45—Determining position by combining measurements of signals from the satellite radio beacon positioning system with a supplementary measurement
    • G01S19/47—Determining position by combining measurements of signals from the satellite radio beacon positioning system with a supplementary measurement the supplementary measurement being an inertial measurement, e.g. tightly coupled inertial
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
    • G01S19/38—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system
    • G01S19/39—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system the satellite radio beacon positioning system transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
    • G01S19/52—Determining velocity
DE60016748T 1999-05-14 2000-05-12 Verfahren und vorrichtung zur bestimmung der vertikalgeschwindigkeit eines flugzeugs Expired - Lifetime DE60016748T2 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US13408999P 1999-05-14 1999-05-14
US134089P 1999-05-14
PCT/US2000/013169 WO2000070354A1 (en) 1999-05-14 2000-05-12 Method and apparatus for determining the vertical speed of an aircraft

Publications (2)

Publication Number Publication Date
DE60016748D1 true DE60016748D1 (de) 2005-01-20
DE60016748T2 DE60016748T2 (de) 2005-12-08

Family

ID=22461727

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60016748T Expired - Lifetime DE60016748T2 (de) 1999-05-14 2000-05-12 Verfahren und vorrichtung zur bestimmung der vertikalgeschwindigkeit eines flugzeugs

Country Status (5)

Country Link
US (2) US6324448B1 (de)
EP (1) EP1190261B1 (de)
AT (1) ATE285077T1 (de)
DE (1) DE60016748T2 (de)
WO (1) WO2000070354A1 (de)

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2000070354A1 (en) * 1999-05-14 2000-11-23 Honeywell International Inc. Method and apparatus for determining the vertical speed of an aircraft
US6427122B1 (en) * 2000-12-23 2002-07-30 American Gnc Corporation Positioning and data integrating method and system thereof
US6522298B1 (en) * 2001-04-12 2003-02-18 Garmin Ltd. Device and method for calibrating and improving the accuracy of barometric altimeters with GPS-derived altitudes
FR2840073B1 (fr) * 2002-05-23 2004-07-16 Eurocopter France Procede et dispositif pour estimer au moins la vitesse verticale d'un aeronef, en particulier d'un aeronef a voilure tournante
FR2852683B1 (fr) * 2003-03-19 2005-05-20 Airbus France Procede et dispositif d'aide au pilotage d'un aeronef lors d'une approche de non precision pendant une phase d'atterrissage.
US7970501B2 (en) * 2005-03-08 2011-06-28 Honeywell International Inc. Methods and systems utilizing true airspeed to improve vertical velocity accuracy
US9099012B2 (en) * 2005-03-14 2015-08-04 Cubic Corporation Adjustment of altitude measurements
US8794970B2 (en) * 2005-03-14 2014-08-05 Steven G. Testrake Control systems to emulate jet aircraft in reciprocating engine-powered trainers
US8784107B2 (en) * 2005-03-14 2014-07-22 Cubic Corporation Flight training system
US7501981B2 (en) * 2005-11-18 2009-03-10 Texas Instruments Incorporated Methods and apparatus to detect and correct integrity failures in satellite positioning system receivers
US7328104B2 (en) * 2006-05-17 2008-02-05 Honeywell International Inc. Systems and methods for improved inertial navigation
FR2938683B1 (fr) * 2008-11-14 2012-06-15 Airbus France Procede et systeme d'evitement de terrain pour un aeronef
DE102009002314A1 (de) * 2009-04-09 2010-07-08 Robert Bosch Gmbh Ebenenfinder
US9671783B2 (en) * 2010-05-25 2017-06-06 Airbus Operations (Sas) Automatic method and device for aiding the piloting of an airplane
US20130190951A1 (en) * 2012-01-20 2013-07-25 Sandel Avionics, Inc. Pressure altitude stabilization
FI124586B (fi) 2012-02-03 2014-10-31 Suunto Oy Menetelmä ja laite korkeuden määrittämiseksi
US8914164B1 (en) * 2013-08-02 2014-12-16 Honeywell International Inc. System and method for computing mach number and true airspeed
US9096330B2 (en) * 2013-08-02 2015-08-04 Honeywell International Inc. System and method for computing MACH number and true airspeed
US10215862B2 (en) 2014-04-07 2019-02-26 Honeywell International Inc. Systems and methods for a code carrier divergence high-pass filter monitor
US20190108760A1 (en) * 2017-10-10 2019-04-11 Honeywell International Inc. System and method for developing and maintaining temperature-compensated altitude information
US10843791B2 (en) * 2018-05-16 2020-11-24 Textron Innovations Inc. System and method for controlling rotorcraft
US11312480B2 (en) 2018-06-01 2022-04-26 Textron Innovations Inc. System and method for controlling rotorcraft
US10816999B2 (en) 2018-06-01 2020-10-27 Textron Innovations Inc. System and method for controlling rotorcraft
GB2588579A (en) * 2019-10-09 2021-05-05 Airbus Operations Ltd Speed determination system
KR102367834B1 (ko) * 2021-05-14 2022-02-25 한화시스템(주) 항공기의 성능 개선을 위한 고도 신호 처리 장치 및 그 방법

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4326253A (en) * 1980-03-31 1982-04-20 The Boeing Company Lift control system for aircraft vertical path guidance
US4490794A (en) * 1982-01-18 1984-12-25 Sperry Corporation Altitude preselect system for aircraft without air data computer
US4882697A (en) * 1987-04-16 1989-11-21 Honeywell Inc. Stabilization control circuit for vertical position in an inertial navigator
US5101356A (en) * 1989-11-21 1992-03-31 Unisys Corporation Moving vehicle attitude measuring system
GB2245445A (en) * 1990-06-18 1992-01-02 Philips Electronic Associated Method of and apparatus for obtaining vehicle heading information
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
US5714948A (en) * 1993-05-14 1998-02-03 Worldwide Notifications Systems, Inc. Satellite based aircraft traffic control system
JPH0743446A (ja) * 1993-08-02 1995-02-14 Aisin Seiki Co Ltd Ｇｐｓ衛星デ−タの検証装置
FR2730841B1 (fr) * 1995-02-17 1997-04-25 Sextant Avionique Procede et dispositif de surveillance et de guidage d'aeronef pour atterrissage de precision
US5839080B1 (en) * 1995-07-31 2000-10-17 Allied Signal 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
US6020832A (en) * 1996-08-05 2000-02-01 Jensen; David D. Method and apparatus of automatically monitoring aircraft altitude
US6088653A (en) * 1996-12-31 2000-07-11 Sheikh; Suneel I. Attitude determination method and system
US5841537A (en) * 1997-08-11 1998-11-24 Rockwell International Synthesized attitude and heading inertial reference
US6216064B1 (en) * 1998-02-24 2001-04-10 Alliedsignal Inc. Method and apparatus for determining altitude
US6262679B1 (en) * 1999-04-08 2001-07-17 Honeywell International Inc. Midair collision avoidance system
WO2000070354A1 (en) * 1999-05-14 2000-11-23 Honeywell International Inc. Method and apparatus for determining the vertical speed of an aircraft
US6205376B1 (en) * 1999-06-22 2001-03-20 Rockwell Collins, Inc. Blocked pitot-static monitor
US6298286B1 (en) * 1999-12-17 2001-10-02 Rockwell Collins Method of preventing potentially hazardously misleading attitude data
US6298287B1 (en) * 2000-07-24 2001-10-02 Litton Systems, Inc. System and method of compensating for pressure sensor errors and noise in inertial vertical loop data

Also Published As

Publication number Publication date
US20020032504A1 (en) 2002-03-14
ATE285077T1 (de) 2005-01-15
WO2000070354A1 (en) 2000-11-23
US6324448B1 (en) 2001-11-27
DE60016748T2 (de) 2005-12-08
US6430479B1 (en) 2002-08-06
EP1190261B1 (de) 2004-12-15
EP1190261A1 (de) 2002-03-27

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