AU2002230906A1 - Receiver-autonomous vertical integrity monitoring - Google Patents

Receiver-autonomous vertical integrity monitoring

Info

Publication number
AU2002230906A1
AU2002230906A1 AU2002230906A AU3090602A AU2002230906A1 AU 2002230906 A1 AU2002230906 A1 AU 2002230906A1 AU 2002230906 A AU2002230906 A AU 2002230906A AU 3090602 A AU3090602 A AU 3090602A AU 2002230906 A1 AU2002230906 A1 AU 2002230906A1
Authority
AU
Australia
Prior art keywords
receiver
integrity monitoring
vertical integrity
autonomous vertical
autonomous
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.)
Abandoned
Application number
AU2002230906A
Inventor
Robert C. Hilb
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.)
United Parcel Service of America Inc
Original Assignee
United Parcel Service of America Inc
United Parcel Service 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 United Parcel Service of America Inc, United Parcel Service Inc filed Critical United Parcel Service of America Inc
Publication of AU2002230906A1 publication Critical patent/AU2002230906A1/en
Abandoned legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • 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
AU2002230906A 2000-12-15 2001-12-13 Receiver-autonomous vertical integrity monitoring Abandoned AU2002230906A1 (en)

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
US25593200P 2000-12-15 2000-12-15
US60/255,932 2000-12-15
US10/016,511 US6711478B2 (en) 2000-12-15 2001-12-10 Receiver-autonomous vertical integrity monitoring
US10/016,511 2001-12-10
PCT/US2001/048606 WO2002048812A2 (en) 2000-12-15 2001-12-13 Receiver-autonomous vertical integrity monitoring

Publications (1)

Publication Number Publication Date
AU2002230906A1 true AU2002230906A1 (en) 2002-06-24

Family

ID=26688695

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2002230906A Abandoned AU2002230906A1 (en) 2000-12-15 2001-12-13 Receiver-autonomous vertical integrity monitoring

Country Status (8)

Country Link
US (1) US6711478B2 (en)
EP (1) EP1342139A2 (en)
JP (1) JP2004522947A (en)
CN (1) CN1481522A (en)
AU (1) AU2002230906A1 (en)
CA (1) CA2431801A1 (en)
MX (1) MXPA03005341A (en)
WO (1) WO2002048812A2 (en)

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US20050107929A1 (en) * 2001-09-01 2005-05-19 Bayerische Motoren Werke Ag Method, device and computer product for updating data of a control device
US6847893B1 (en) * 2003-01-22 2005-01-25 Trimble Navigation, Ltd Horizontal/vertical exclusion level determination scheme for RAIM fault detection and exclusion implementation
US6896220B2 (en) * 2003-05-23 2005-05-24 Raytheon Company Munition with integrity gated go/no-go decision
US6796213B1 (en) * 2003-05-23 2004-09-28 Raytheon Company Method for providing integrity bounding of weapons
US7019687B1 (en) * 2004-11-22 2006-03-28 Raytheon Company Methods and apparatus for satellite integrity messaging
DE602005021398D1 (en) * 2004-12-16 2010-07-01 Raytheon Co DETERMINATION OF A PROGNOSTICED PERFORMANCE OF A NAVIGATION SYSTEM
FR2888636B1 (en) * 2005-07-13 2007-09-28 Airbus France Sas DEVICE FOR AIDING AN APPROACH WITH VERTICAL GUIDE FOR AN AIRCRAFT
EP1777159A1 (en) * 2005-10-20 2007-04-25 Astrium GmbH Arrangement and method for determining position and attitude of a flight vehicle, in particular of a space vehicle
DE602005012279D1 (en) * 2005-10-25 2009-02-26 Saab Ab Height control system for an aircraft
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
US20070239326A1 (en) * 2006-04-05 2007-10-11 Honeywell International, Inc. Systems and methods for monitoring an altitude in a flight vehicle
FR2902081B1 (en) * 2006-06-12 2008-07-11 Airbus France Sas LANDING ASSISTANCE METHOD AND DEVICE FOR AIRCRAFT
CN100442077C (en) * 2007-07-12 2008-12-10 北京航空航天大学 Usable forcasting method for receiver autonomic excellent monitoring
US8014948B2 (en) * 2007-12-07 2011-09-06 Honeywell International Inc. Navigation system with apparatus for detecting accuracy failures
US20090182493A1 (en) * 2008-01-15 2009-07-16 Honeywell International, Inc. Navigation system with apparatus for detecting accuracy failures
US20090182494A1 (en) * 2008-01-15 2009-07-16 Honeywell International, Inc. Navigation system with apparatus for detecting accuracy failures
US20090182495A1 (en) * 2008-01-15 2009-07-16 Honeywell International, Inc. Navigation system with apparatus for detecting accuracy failures
US8615337B1 (en) * 2008-09-25 2013-12-24 Rockwell Collins, Inc. System supporting flight operations under instrument meteorological conditions using precision course guidance
JP4926213B2 (en) * 2009-07-15 2012-05-09 株式会社京三製作所 Train control device
US8494693B2 (en) 2009-08-05 2013-07-23 The Boeing Company Vertical required navigation performance containment with radio altitude
US20110118979A1 (en) * 2009-11-19 2011-05-19 Robert Bosch Gmbh Automotive location data integrity
FR2964466B1 (en) * 2010-09-06 2012-10-12 Airbus Operations Sas METHOD AND DEVICE FOR AUTOMATICALLY DETECTING AN ERRONEOUS HEIGHT VALUE SUPPLIED BY A RADIOALTIMETER MOUNTED ON AN AIRCRAFT.
JP6015030B2 (en) * 2012-03-02 2016-10-26 日本電気株式会社 Airway management device and airway management method
US9341718B2 (en) 2012-09-07 2016-05-17 Honeywell International Inc. Method and system for providing integrity for hybrid attitude and true heading
FR2998378B1 (en) 2012-11-16 2016-01-29 Thales Sa METHOD OF ESTIMATING THE ERROR LEVEL OF SATELLITE GEOLOCATION MEASUREMENTS AND MONITORING THE RELIABILITY OF SATELLITE ESTIMATES AND DEVICE THEREOF
US9051061B2 (en) * 2012-12-14 2015-06-09 Safe Flight Instrument Corporation Systems and methods for safely landing an aircraft
FR3008818B1 (en) * 2013-07-22 2015-08-14 Airbus Operations Sas DEVICE AND METHOD FOR PREDICTING THE PRECISION, THE INTEGRITY AND AVAILABILITY OF THE POSITION OF AN AIRCRAFT ALONG A TRACK.
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
US10012731B2 (en) 2014-04-03 2018-07-03 Johnson Outdoors Inc. Sonar mapping system
US9346552B2 (en) 2014-04-11 2016-05-24 Safe Flight Instrument Corporation Autothrottle retard control
FR3024250B1 (en) * 2014-07-23 2016-12-09 Airbus Operations Sas METHOD AND DEVICE FOR AUTOMATICALLY ENGAGING AUTOMATED EMERGENCY DESCENT OF AN AIRCRAFT
JP6368600B2 (en) * 2014-09-19 2018-08-01 株式会社エヌ・ティ・ティ・データ Control alarm device, air traffic control system, control alarm method, and program
CN104898134B (en) * 2015-05-27 2018-02-23 中国科学院嘉兴微电子与系统工程中心 A kind of satellite fix integrity detection means and its algorithm
US20170008639A1 (en) 2015-07-08 2017-01-12 Safe Flight Instrument Corporation Aircraft turbulence detection
US9738399B2 (en) * 2015-07-29 2017-08-22 Hon Hai Precision Industry Co., Ltd. Unmanned aerial vehicle control method and unmanned aerial vehicle using same
US10545235B2 (en) 2016-11-01 2020-01-28 Johnson Outdoors Inc. Sonar mapping system
RU2659376C1 (en) * 2017-03-23 2018-06-29 Акционерное общество "Ордена Трудового Красного Знамени Всероссийский научно-исследовательский институт радиоаппаратуры" (АО "ВНИИРА") Descending space objects or their devices coordinates monitoring in the earth atmosphere and their dispatching control system
WO2020262528A1 (en) * 2019-06-27 2020-12-30 株式会社Ｎｔｔドコモ Information processing device, and information processing method
CN111679298B (en) * 2020-05-09 2023-05-09 香港理工大学深圳研究院 Integrity monitoring method and device of navigation system and electronic equipment
US11555930B2 (en) 2020-06-24 2023-01-17 Honeywell Aerospace Sas Split vertical advanced receiver autonomous integrity monitoring

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US5600329A (en) 1995-06-30 1997-02-04 Honeywell Inc. Differential satellite positioning system ground station with integrity monitoring
US5839080B1 (en) * 1995-07-31 2000-10-17 Allied Signal Inc Terrain awareness system
US6020832A (en) * 1996-08-05 2000-02-01 Jensen; David D. Method and apparatus of automatically monitoring aircraft altitude
US5923286A (en) 1996-10-23 1999-07-13 Honeywell Inc. GPS/IRS global position determination method and apparatus with integrity loss provisions
GB2322611B (en) * 1997-02-26 2001-03-21 British Aerospace Apparatus for indicating air traffic and terrain collision threat to an aircraft
US6094607A (en) * 1998-11-27 2000-07-25 Litton Systems Inc. 3D AIME™ aircraft navigation
US5969670A (en) * 1998-01-22 1999-10-19 Trimble Navigation Limited Inexpensive monitoring technique for achieving high level integrity monitoring for differential GPS
US6281836B1 (en) 1999-05-21 2001-08-28 Trimble Navigation Ltd Horizontal/vertical protection level adjustment scheme for RAIM with baro measurements
US6317688B1 (en) 2000-01-31 2001-11-13 Rockwell Collins Method and apparatus for achieving sole means navigation from global navigation satelite systems
US20020072832A1 (en) * 2000-12-11 2002-06-13 Bachinski Thomas J. System and method of determining an altitude of an aircraft using barometric pressure measurements
US6799116B2 (en) * 2000-12-15 2004-09-28 Trimble Navigation Limited GPS correction methods, apparatus and signals

Also Published As

Publication number Publication date
WO2002048812A2 (en) 2002-06-20
US6711478B2 (en) 2004-03-23
EP1342139A2 (en) 2003-09-10
MXPA03005341A (en) 2003-10-06
CN1481522A (en) 2004-03-10
WO2002048812A3 (en) 2002-11-21
WO2002048812A9 (en) 2003-04-24
US20020077731A1 (en) 2002-06-20
CA2431801A1 (en) 2002-06-20
JP2004522947A (en) 2004-07-29

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