BR112018068749A2 - método e sistema para determinar as correções de satélite de navegação, e, mídia de armazenamento legível por computador não transitória. - Google Patents
método e sistema para determinar as correções de satélite de navegação, e, mídia de armazenamento legível por computador não transitória.Info
- Publication number
- BR112018068749A2 BR112018068749A2 BR112018068749-9A BR112018068749A BR112018068749A2 BR 112018068749 A2 BR112018068749 A2 BR 112018068749A2 BR 112018068749 A BR112018068749 A BR 112018068749A BR 112018068749 A2 BR112018068749 A2 BR 112018068749A2
- Authority
- BR
- Brazil
- Prior art keywords
- satellite
- wide
- receivers
- navigational
- computer readable
- Prior art date
Links
- 238000012937 correction Methods 0.000 title abstract 3
- 238000000034 method Methods 0.000 title 1
- 230000001052 transient effect Effects 0.000 title 1
- 238000005259 measurement Methods 0.000 abstract 2
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
- G01S19/38—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
- G01S19/40—Correcting position, velocity or attitude
- G01S19/41—Differential correction, e.g. DGPS [differential GPS]
-
- 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
- G01S19/03—Cooperating elements; Interaction or communication between different cooperating elements or between cooperating elements and receivers
- G01S19/07—Cooperating elements; Interaction or communication between different cooperating elements or between cooperating elements and receivers providing data for correcting measured positioning data, e.g. DGPS [differential GPS] or ionosphere corrections
- G01S19/071—DGPS corrections
-
- 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
- G01S19/03—Cooperating elements; Interaction or communication between different cooperating elements or between cooperating elements and receivers
- G01S19/07—Cooperating elements; Interaction or communication between different cooperating elements or between cooperating elements and receivers providing data for correcting measured positioning data, e.g. DGPS [differential GPS] or ionosphere corrections
- G01S19/072—Ionosphere corrections
-
- 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
- G01S19/32—Multimode operation in a single same satellite system, e.g. GPS L1/L2
-
- 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
- G01S19/43—Determining position using carrier phase measurements, e.g. kinematic positioning; using long or short baseline interferometry
- G01S19/44—Carrier phase ambiguity resolution; Floating ambiguity; LAMBDA [Least-squares AMBiguity Decorrelation Adjustment] method
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)
Abstract
um sistema de geração de correções de satélite recebe informação de medição do receptor de referência a partir de uma pluralidade de receptores de referência em locais estabelecidos (402). de acordo com a informação de medição do receptor de referência recebida, e locais estabelecidos dos receptores de referência, o sistema determina as soluções de navegação de rota larga para a pluralidade de receptores de referência (404). o sistema também determina os agrupamentos de ambiguidades flutuantes de rota larga com diferença única (sd) (408). um valor de tendência rota larga do satélite para cada satélite de uma pluralidade de satélites é inicialmente determinado de acordo com porções fracionárias das ambiguidades flutuantes de rota larga sd nos agrupamentos e critérios de ajuste de alcance excessivo (412 e 414). um conjunto de correções de satélite de navegação para cada satélite, incluindo o valor de tendência rota larga do satélite para cada satélite, é gerado e transmitido para receptores de navegação para uso na determinação de locais dos receptores de navegação (416 e 418).
Applications Claiming Priority (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201662310545P | 2016-03-18 | 2016-03-18 | |
US62/310,545 | 2016-03-18 | ||
US15/448,474 | 2017-03-02 | ||
US15/448,474 US10564294B2 (en) | 2016-03-18 | 2017-03-02 | Navigation satellite wide-lane bias determination and over-range adjustment system and method |
PCT/US2017/021742 WO2017160618A1 (en) | 2016-03-18 | 2017-03-10 | Navigation satellite wide-lane bias determination and over-range adjustment system and method |
Publications (1)
Publication Number | Publication Date |
---|---|
BR112018068749A2 true BR112018068749A2 (pt) | 2019-04-09 |
Family
ID=59848279
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112018068749-9A BR112018068749A2 (pt) | 2016-03-18 | 2017-03-10 | método e sistema para determinar as correções de satélite de navegação, e, mídia de armazenamento legível por computador não transitória. |
BR112018068762-6A BR112018068762A2 (pt) | 2016-03-18 | 2017-03-10 | método e sistema para determinar as correções de satélite de navegação, e, mídia de armazenamento legível por computador não transitória. |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112018068762-6A BR112018068762A2 (pt) | 2016-03-18 | 2017-03-10 | método e sistema para determinar as correções de satélite de navegação, e, mídia de armazenamento legível por computador não transitória. |
Country Status (5)
Country | Link |
---|---|
US (2) | US10338232B2 (pt) |
EP (2) | EP3430437B1 (pt) |
CN (2) | CN109154670B (pt) |
BR (2) | BR112018068749A2 (pt) |
WO (2) | WO2017160618A1 (pt) |
Families Citing this family (12)
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US10338232B2 (en) | 2016-03-18 | 2019-07-02 | Deere & Company | Navigation satellite wide-lane bias determination system and method |
CN108196284B (zh) * | 2018-01-20 | 2021-07-27 | 中国人民解放军61540部队 | 一种进行星间单差模糊度固定的gnss网数据处理方法 |
US12099125B2 (en) | 2018-06-25 | 2024-09-24 | Deere & Company | Adaptive estimation of GNSS satellite biases |
CN111025340B (zh) * | 2018-10-10 | 2022-02-08 | 千寻位置网络有限公司 | 频间偏差一致性的评估方法及装置、监控设备 |
CN111142127B (zh) * | 2018-11-02 | 2023-04-21 | 千寻位置网络有限公司 | 周跳探测方法及其装置 |
US12016257B2 (en) | 2020-02-19 | 2024-06-25 | Sabanto, Inc. | Methods for detecting and clearing debris from planter gauge wheels, closing wheels and seed tubes |
US11808861B2 (en) * | 2021-01-31 | 2023-11-07 | Deere & Company | Adaptive estimation of GNSS satellite biases |
US11947022B2 (en) * | 2021-03-30 | 2024-04-02 | Mitsubishi Electric Research Laboratories, Inc | Cooperative state tracking of multiple vehicles using individual and joint estimations |
CN113281794A (zh) * | 2021-04-27 | 2021-08-20 | 中国人民解放军陆军勤务学院 | 一种并行估计星间单差宽巷fcb的方法 |
CN114355417B (zh) * | 2021-12-08 | 2023-09-01 | 杭州电子科技大学 | 顾及伪距多径、轨道及数据类型的三频周跳探测修复法 |
US12032077B2 (en) | 2022-03-11 | 2024-07-09 | Deere & Company | System and method for compensating for scintillation and for facilitation of long-baseline RTK |
CN117952328B (zh) * | 2024-03-27 | 2024-06-25 | 江苏端木软件技术有限公司 | 一种基于数据分析的自动化测试系统及方法 |
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US5991691A (en) | 1997-02-20 | 1999-11-23 | Raytheon Aircraft Corporation | System and method for determining high accuracy relative position solutions between two moving platforms |
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-
2017
- 2017-03-02 US US15/448,457 patent/US10338232B2/en active Active
- 2017-03-02 US US15/448,474 patent/US10564294B2/en active Active
- 2017-03-10 BR BR112018068749-9A patent/BR112018068749A2/pt unknown
- 2017-03-10 CN CN201780018359.3A patent/CN109154670B/zh active Active
- 2017-03-10 BR BR112018068762-6A patent/BR112018068762A2/pt unknown
- 2017-03-10 CN CN201780018282.XA patent/CN109219762B/zh active Active
- 2017-03-10 WO PCT/US2017/021742 patent/WO2017160618A1/en active Application Filing
- 2017-03-10 EP EP17767201.1A patent/EP3430437B1/en active Active
- 2017-03-10 WO PCT/US2017/021738 patent/WO2017160617A1/en active Application Filing
- 2017-03-10 EP EP17767202.9A patent/EP3430431B1/en active Active
Also Published As
Publication number | Publication date |
---|---|
CN109219762B (zh) | 2023-08-29 |
CN109219762A (zh) | 2019-01-15 |
WO2017160617A1 (en) | 2017-09-21 |
EP3430437B1 (en) | 2020-08-12 |
US10564294B2 (en) | 2020-02-18 |
EP3430431A4 (en) | 2020-01-01 |
WO2017160618A1 (en) | 2017-09-21 |
EP3430431A1 (en) | 2019-01-23 |
EP3430437A4 (en) | 2020-01-01 |
BR112018068762A2 (pt) | 2019-04-09 |
US20170269225A1 (en) | 2017-09-21 |
EP3430437A1 (en) | 2019-01-23 |
EP3430431B1 (en) | 2021-03-03 |
CN109154670B (zh) | 2023-06-02 |
US10338232B2 (en) | 2019-07-02 |
US20170269223A1 (en) | 2017-09-21 |
CN109154670A (zh) | 2019-01-04 |
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