IN2014DE03240A - - Google Patents

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Publication number
IN2014DE03240A
IN2014DE03240A IN3240DE2014A IN2014DE03240A IN 2014DE03240 A IN2014DE03240 A IN 2014DE03240A IN 3240DE2014 A IN3240DE2014 A IN 3240DE2014A IN 2014DE03240 A IN2014DE03240 A IN 2014DE03240A
Authority
IN
India
Prior art keywords
satellites
sub
criterion
satisfies
calculate
Prior art date
Application number
Inventor
Dunik Jindrich
Orejas Martin
Kana Zdenek
Original Assignee
Honeywell Int 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 Int Inc filed Critical Honeywell Int Inc
Publication of IN2014DE03240A publication Critical patent/IN2014DE03240A/en

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Classifications

    • 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
    • G01S19/24—Acquisition or tracking or demodulation of signals transmitted by the system
    • G01S19/28—Satellite selection
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Position Fixing By Use Of Radio Waves (AREA)
  • Navigation (AREA)

Abstract

In one embodiment, a method for selecting a sub-set of satellites from a set of N satellites is provided. The method includes recursively evaluating each sub-set of N-P satellites of a set of N satellites. If only one sub-set satisfies one or more first criterion, then the one subset that satisfies the one or more first criterions is selected. If, however, more than one sub-set satisfies the one or more first criterion, then the sub-sets that satisfy the one or more first criterion are evaluated with respect to one or more second criterion and the one sub-set that optimizes the one or more second criterion is selected. Once the selected set of N satellites is equal to the number of satellites from which a receiver is configured to calculate a navigation solution, then that selected set of N satellites is used to calculate a navigation solution.
IN3240DE2014 2013-10-27 2014-11-10 IN2014DE03240A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US14/091,441 US9766346B2 (en) 2013-10-27 2013-10-27 Multiple-criterion based global navigation satellite sub-set recursive selection

Publications (1)

Publication Number Publication Date
IN2014DE03240A true IN2014DE03240A (en) 2015-09-25

Family

ID=51868801

Family Applications (1)

Application Number Title Priority Date Filing Date
IN3240DE2014 IN2014DE03240A (en) 2013-10-27 2014-11-10

Country Status (7)

Country Link
US (1) US9766346B2 (en)
EP (1) EP2881759B1 (en)
JP (1) JP2015102546A (en)
CN (1) CN104678410A (en)
CA (1) CA2869861C (en)
IN (1) IN2014DE03240A (en)
RU (1) RU2014147621A (en)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20160247392A1 (en) * 2014-10-27 2016-08-25 Umm Al-Qura University A method and system for 3d position estimation of an object using time of arrival measurements
US9885788B2 (en) * 2015-03-16 2018-02-06 Honeywell International Inc. Satellite subset selection for use in monitoring the integrity of computed navigation solutions
JP6545273B2 (en) * 2015-09-17 2019-07-17 三菱電機株式会社 Positioning satellite selection device, positioning information transmission device and positioning system
US10495761B2 (en) 2015-11-13 2019-12-03 Honeywell International Inc. Smart satellite distribution into ARAIM clusters for use in monitoring integrity of computed navigation solutions
CN106125101A (en) * 2016-08-17 2016-11-16 北京航空航天大学 The assessment processing method and processing device of ARAIM availability based on the Big Dipper
US10613233B2 (en) * 2016-09-21 2020-04-07 Honeywell International Inc. ARAIM clustering distribution improvement
US10416315B2 (en) 2017-03-07 2019-09-17 Honeywell International Inc. False alarm distribution in advanced receiver autonomous integrity monitoring
CN108627859B (en) * 2018-05-10 2021-05-28 上海海积信息科技股份有限公司 Reliability analysis method and device for RTK algorithm result
CN111487660B (en) * 2020-04-24 2022-07-26 北京航空航天大学 High-precision real-time micro-nano satellite cluster navigation method
US11555930B2 (en) * 2020-06-24 2023-01-17 Honeywell Aerospace Sas Split vertical advanced receiver autonomous integrity monitoring
CN114715430B (en) * 2021-03-31 2022-11-08 中国科学院国家空间科学中心 System for multi-satellite automatic linear formation and time-varying baseline generation

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7783425B1 (en) 2005-06-29 2010-08-24 Rockwell Collins, Inc. Integrity-optimized receiver autonomous integrity monitoring (RAIM)
DE102007006612B4 (en) * 2007-02-06 2013-10-24 Astrium Gmbh A method, terminal and computer program product for increasing the availability of a global navigation system
ATE474233T1 (en) 2008-04-21 2010-07-15 Deutsch Zentr Luft & Raumfahrt METHOD FOR OPERATING A SATELLITE NAVIGATION RECEIVER
CN101866010B (en) * 2010-05-28 2013-02-27 北京航空航天大学 Star choosing method for satellite navigation system
EP2864809B9 (en) * 2012-06-20 2017-08-16 Topcon Positioning Systems, Inc. Selection of a subset of global navigation satellite system measurements based on prediction of accuracy of target parameters

Also Published As

Publication number Publication date
RU2014147621A (en) 2016-06-10
US9766346B2 (en) 2017-09-19
CA2869861A1 (en) 2015-05-27
US20150145719A1 (en) 2015-05-28
EP2881759B1 (en) 2016-02-17
CA2869861C (en) 2022-05-10
JP2015102546A (en) 2015-06-04
EP2881759A1 (en) 2015-06-10
CN104678410A (en) 2015-06-03

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