IN2014DE03160A - - Google Patents

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Publication number
IN2014DE03160A
IN2014DE03160A IN3160DE2014A IN2014DE03160A IN 2014DE03160 A IN2014DE03160 A IN 2014DE03160A IN 3160DE2014 A IN3160DE2014 A IN 3160DE2014A IN 2014DE03160 A IN2014DE03160 A IN 2014DE03160A
Authority
IN
India
Prior art keywords
domain
sub
solutions
signals
space
Prior art date
Application number
Other languages
English (en)
Inventor
Kana Zdenek
Dunik Jindrich
Orejas Martin
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 IN2014DE03160A publication Critical patent/IN2014DE03160A/en

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Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO 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
    • G01S19/00Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
    • G01S19/01Satellite radio beacon positioning systems transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
    • G01S19/13Receivers
    • G01S19/20Integrity monitoring, fault detection or fault isolation of space segment
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO 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
    • G01S19/00Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
    • G01S19/38Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system
    • G01S19/39Determining 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
    • G01S19/42Determining position
    • G01S19/421Determining position by combining or switching between position solutions or signals derived from different satellite radio beacon positioning systems; by combining or switching between position solutions or signals derived from different modes of operation in a single system

Landscapes

  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Computer Security & Cryptography (AREA)
  • Position Fixing By Use Of Radio Waves (AREA)
IN3160DE2014 2013-11-27 2014-11-03 IN2014DE03160A (enExample)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US14/092,454 US9784844B2 (en) 2013-11-27 2013-11-27 Architectures for high integrity multi-constellation solution separation

Publications (1)

Publication Number Publication Date
IN2014DE03160A true IN2014DE03160A (enExample) 2015-07-10

Family

ID=51903760

Family Applications (1)

Application Number Title Priority Date Filing Date
IN3160DE2014 IN2014DE03160A (enExample) 2013-11-27 2014-11-03

Country Status (3)

Country Link
US (1) US9784844B2 (enExample)
EP (1) EP2887097B1 (enExample)
IN (1) IN2014DE03160A (enExample)

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US9784844B2 (en) 2013-11-27 2017-10-10 Honeywell International Inc. Architectures for high integrity multi-constellation solution separation
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FR3030058B1 (fr) * 2014-12-11 2016-12-09 Airbus Helicopters Dispositif redondant de capteurs de pilotage pour aeronef a voiture tournante
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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
US10422872B2 (en) 2016-06-01 2019-09-24 Honeywell International Inc. Integrity monitoring of radar altimeters
US10613233B2 (en) * 2016-09-21 2020-04-07 Honeywell International Inc. ARAIM clustering distribution improvement
DE102016225282A1 (de) 2016-12-16 2018-06-21 Continental Automotive Gmbh Verfahren und Vorrichtung zum Ermitteln einer Navigationsposition eines Navigationssystems für ein Kraftfahrzeug sowie Navigationssystem
EP3555665B1 (en) 2016-12-19 2022-08-24 Magellan Systems Japan, Inc. Detection and elimination of gnss spoofing signals with pvt solution estimation
US11585943B2 (en) 2016-12-19 2023-02-21 Magellan Systems Japan, Inc. Detection and elimination of GNSS spoofing signals with PVT solution estimation
US10416315B2 (en) 2017-03-07 2019-09-17 Honeywell International Inc. False alarm distribution in advanced receiver autonomous integrity monitoring
US10760911B2 (en) 2017-03-29 2020-09-01 Honeywell International Inc. Integrity monitoring method for navigation systems with heterogeneous measurements
US10935663B2 (en) * 2017-09-22 2021-03-02 Qualcomm Incorporated Satellite integrity monitoring with crowdsourced mobile device data
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US10578747B2 (en) 2017-12-14 2020-03-03 Swift Navigation, Inc. Systems and methods for reduced-outlier satellite positioning
US10889302B2 (en) 2018-06-27 2021-01-12 Honeywell International Inc. Methods for monitoring the output performance of state estimators in navigation systems
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WO2020223684A1 (en) 2019-05-01 2020-11-05 Swift Navigation, Inc. Systems and methods for high-integrity satellite positioning
US11226418B2 (en) * 2019-06-19 2022-01-18 Novatel Inc. System and method for calculating protection levels for velocity and course over ground
CN114502987B (zh) 2019-08-01 2025-07-25 斯威夫特导航股份有限公司 用于高斯过程增强的gnss校正生成的系统和方法
US11016199B1 (en) 2019-12-11 2021-05-25 Swift Navigation, Inc. System and method for validating GNSS ambiguities
WO2021202004A2 (en) 2020-02-14 2021-10-07 Swift Navigation, Inc. System and method for reconverging gnss position estimates
EP4162300A4 (en) 2020-06-09 2024-07-17 Swift Navigation, Inc. System and method for satellite positioning
CN116261676B (zh) 2020-07-13 2025-10-03 斯威夫特导航股份有限公司 用于确定gnss定位校正的系统和方法
WO2022046317A2 (en) 2020-07-17 2022-03-03 Swift Navigation, Inc. System and method for providing gnss corrections
US11550067B2 (en) 2020-12-17 2023-01-10 Swift Navigation, Inc. System and method for fusing dead reckoning and GNSS data streams
CN113515881B (zh) * 2021-03-23 2023-05-16 北京航空航天大学 一种面向araim应用的低轨卫星增强系统星座配置优化方法
US12153148B2 (en) * 2021-05-17 2024-11-26 Reliable Robotics Corporation Radar altimeter augmented receiver autonomous integrity monitoring in aircraft
US11733397B2 (en) 2021-07-24 2023-08-22 Swift Navigation, Inc. System and method for computing positioning protection levels
US11693120B2 (en) 2021-08-09 2023-07-04 Swift Navigation, Inc. System and method for providing GNSS corrections
WO2023107742A1 (en) 2021-12-10 2023-06-15 Swift Navigation, Inc. System and method for correcting satellite observations
US11906640B2 (en) 2022-03-01 2024-02-20 Swift Navigation, Inc. System and method for fusing sensor and satellite measurements for positioning determination
US11860287B2 (en) 2022-03-01 2024-01-02 Swift Navigation, Inc. System and method for detecting outliers in GNSS observations
CN115062097B (zh) * 2022-06-22 2025-06-20 涟漪位置(广州)科技有限公司 一种定位完好性监测方法、终端及计算机存储介质
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US9547086B2 (en) 2013-03-26 2017-01-17 Honeywell International Inc. Selected aspects of advanced receiver autonomous integrity monitoring application to kalman filter based navigation filter
US9784844B2 (en) 2013-11-27 2017-10-10 Honeywell International Inc. Architectures for high integrity multi-constellation solution separation

Also Published As

Publication number Publication date
EP2887097A3 (en) 2015-12-16
US20150145724A1 (en) 2015-05-28
EP2887097A2 (en) 2015-06-24
EP2887097B1 (en) 2023-04-12
US9784844B2 (en) 2017-10-10

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