BR102013015045B1 - Método, sistema baseado em computador para compensação de latência em um sistema dinâmico e meio legível por computador não transitório - Google Patents

Método, sistema baseado em computador para compensação de latência em um sistema dinâmico e meio legível por computador não transitório Download PDF

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Publication number
BR102013015045B1
BR102013015045B1 BR102013015045-2A BR102013015045A BR102013015045B1 BR 102013015045 B1 BR102013015045 B1 BR 102013015045B1 BR 102013015045 A BR102013015045 A BR 102013015045A BR 102013015045 B1 BR102013015045 B1 BR 102013015045B1
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BR
Brazil
Prior art keywords
parameter data
latency
sensor
processor
computer
Prior art date
Application number
BR102013015045-2A
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English (en)
Portuguese (pt)
Other versions
BR102013015045A2 (pt
Inventor
Steven B. Krogh
Original Assignee
The Boeing Company
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 The Boeing Company filed Critical The Boeing Company
Publication of BR102013015045A2 publication Critical patent/BR102013015045A2/pt
Publication of BR102013015045B1 publication Critical patent/BR102013015045B1/pt

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    • 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
    • G01S19/42—Determining position
    • G01S19/48—Determining position by combining or switching between position solutions derived from the satellite radio beacon positioning system and position solutions derived from a further system
    • G01S19/49—Determining position by combining or switching between position solutions derived from the satellite radio beacon positioning system and position solutions derived from a further system whereby the further system is an inertial position system, e.g. loosely-coupled
    • 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
    • G01S19/48—Determining position by combining or switching between position solutions derived from the satellite radio beacon positioning system and position solutions derived from a further system
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G—PHYSICS
    • G06—COMPUTING OR CALCULATING; COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F17/00—Digital computing or data processing equipment or methods, specially adapted for specific functions

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  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Position Fixing By Use Of Radio Waves (AREA)
  • Navigation (AREA)
  • Feedback Control In General (AREA)
  • Complex Calculations (AREA)
  • Image Processing (AREA)
  • Apparatus For Radiation Diagnosis (AREA)
BR102013015045-2A 2012-06-15 2013-06-17 Método, sistema baseado em computador para compensação de latência em um sistema dinâmico e meio legível por computador não transitório BR102013015045B1 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/524,084 2012-06-15
US13/524,084 US8996598B2 (en) 2012-06-15 2012-06-15 Latency compensation

Publications (2)

Publication Number Publication Date
BR102013015045A2 BR102013015045A2 (pt) 2015-06-23
BR102013015045B1 true BR102013015045B1 (pt) 2022-04-19

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
BR102013015045-2A BR102013015045B1 (pt) 2012-06-15 2013-06-17 Método, sistema baseado em computador para compensação de latência em um sistema dinâmico e meio legível por computador não transitório

Country Status (7)

Country Link
US (1) US8996598B2 (enExample)
EP (1) EP2674781B1 (enExample)
JP (1) JP6465539B2 (enExample)
CN (1) CN103514316B (enExample)
BR (1) BR102013015045B1 (enExample)
CA (1) CA2811756C (enExample)
RU (1) RU2633034C2 (enExample)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8996598B2 (en) * 2012-06-15 2015-03-31 The Boeing Company Latency compensation
US9489045B2 (en) * 2015-03-26 2016-11-08 Honeywell International Inc. Methods and apparatus for providing a snapshot truthing system for a tracker
US11237002B2 (en) * 2016-03-28 2022-02-01 Aisin Corporation Server device, communication terminal, route retrieval system, and computer program
JP6772809B2 (ja) * 2016-12-14 2020-10-21 株式会社Ihi 情報処理装置及び情報処理方法
US10425622B2 (en) 2017-07-18 2019-09-24 The United States Of America As Represented By The Secretary Of The Army Method of generating a predictive display for tele-operation of a remotely-operated ground vehicle
US11238200B2 (en) * 2018-03-05 2022-02-01 Textron Innovations Inc. Targeting system and simulator therefor
US10773666B2 (en) * 2018-05-08 2020-09-15 Infineon Technologies Ag High speed sensor interface
CN110647158B (zh) * 2019-09-19 2022-07-05 北京控制工程研究所 一种考虑时延特性的航天器敏捷机动控制误差补偿方法
EP3861439A4 (en) 2019-12-20 2021-12-15 Baidu.com Times Technology (Beijing) Co., Ltd. DYNAMIC MODEL WITH ACTUATION LATENCY
EP4285615B1 (en) * 2021-01-27 2024-11-20 Signify Holding B.V. Rf-based sensing with consistent latency

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6133871A (en) * 1995-10-09 2000-10-17 Snaptrack, Inc. GPS receiver having power management
US6549829B1 (en) 2001-10-31 2003-04-15 The Boeing Company Skipping filter for inertially augmented landing system
JP3852842B2 (ja) * 2003-05-21 2006-12-06 長崎県 飛翔体の位置姿勢計測装置
US7289906B2 (en) 2004-04-05 2007-10-30 Oregon Health & Science University Navigation system applications of sigma-point Kalman filters for nonlinear estimation and sensor fusion
DE602005025703D1 (de) * 2005-07-29 2011-02-10 Sensata Technologies Inc Kompensationsanordnung und verfahren zu ihrem betrieb
US7579984B2 (en) * 2005-11-23 2009-08-25 The Boeing Company Ultra-tightly coupled GPS and inertial navigation system for agile platforms
US7962255B2 (en) 2006-12-12 2011-06-14 The Boeing Company System and method for estimating inertial acceleration bias errors
US8774950B2 (en) * 2008-01-22 2014-07-08 Carnegie Mellon University Apparatuses, systems, and methods for apparatus operation and remote sensing
US8412456B2 (en) 2008-11-06 2013-04-02 Texas Instruments Incorporated Loosely-coupled integration of global navigation satellite system and inertial navigation system: speed scale-factor and heading bias calibration
EP2192385A1 (en) * 2008-11-26 2010-06-02 Nederlandse Organisatie voor toegepast- natuurwetenschappelijk onderzoek TNO Signal processing module, navigation device with the signal processing module, vehicle provided with a navigation device and method of providing navigation data
US10054444B2 (en) * 2009-05-29 2018-08-21 Qualcomm Incorporated Method and apparatus for accurate acquisition of inertial sensor data
RU2009145970A (ru) * 2009-12-08 2011-06-20 Открытое акционерное общество "Концерн "Центральный научно-исследовательский институт "Электроприбор" (RU) Интегрированная инерциально-спутниковая система ориентации и навигации
US8996598B2 (en) * 2012-06-15 2015-03-31 The Boeing Company Latency compensation

Also Published As

Publication number Publication date
CN103514316B (zh) 2018-12-11
EP2674781A3 (en) 2014-06-18
US8996598B2 (en) 2015-03-31
CA2811756C (en) 2015-12-29
CA2811756A1 (en) 2013-12-15
EP2674781B1 (en) 2019-04-10
JP6465539B2 (ja) 2019-02-06
BR102013015045A2 (pt) 2015-06-23
CN103514316A (zh) 2014-01-15
JP2014002147A (ja) 2014-01-09
RU2013127127A (ru) 2014-12-20
US20130339415A1 (en) 2013-12-19
RU2633034C2 (ru) 2017-10-11
EP2674781A2 (en) 2013-12-18

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Date Code Title Description
B03A Publication of a patent application or of a certificate of addition of invention [chapter 3.1 patent gazette]
B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 17/06/2013, OBSERVADAS AS CONDICOES LEGAIS.