WO2004063762A1 - Dual redundant gps anti-jam air vehicle navigation system - Google Patents
Dual redundant gps anti-jam air vehicle navigation system Download PDFInfo
- Publication number
- WO2004063762A1 WO2004063762A1 PCT/US2003/040659 US0340659W WO2004063762A1 WO 2004063762 A1 WO2004063762 A1 WO 2004063762A1 US 0340659 W US0340659 W US 0340659W WO 2004063762 A1 WO2004063762 A1 WO 2004063762A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- global positioning
- interference
- interference suppression
- positioning system
- navigation
- Prior art date
Links
Classifications
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04K—SECRET COMMUNICATION; JAMMING OF COMMUNICATION
- H04K3/00—Jamming of communication; Counter-measures
- H04K3/20—Countermeasures against jamming
- H04K3/22—Countermeasures against jamming including jamming detection and monitoring
- H04K3/224—Countermeasures against jamming including jamming detection and monitoring with countermeasures at transmission and/or reception of the jammed signal, e.g. stopping operation of transmitter or receiver, nulling or enhancing transmitted power in direction of or at frequency of jammer
- H04K3/228—Elimination in the received signal of jamming or of data corrupted by jamming
-
- 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
- G01S1/00—Beacons or beacon systems transmitting signals having a characteristic or characteristics capable of being detected by non-directional receivers and defining directions, positions, or position lines fixed relatively to the beacon transmitters; Receivers co-operating therewith
- G01S1/02—Beacons or beacon systems transmitting signals having a characteristic or characteristics capable of being detected by non-directional receivers and defining directions, positions, or position lines fixed relatively to the beacon transmitters; Receivers co-operating therewith using radio waves
- G01S1/04—Details
-
- 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
- G01S19/21—Interference related issues ; Issues related to cross-correlation, spoofing or other methods of denial of service
-
- 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
- G01S19/35—Constructional details or hardware or software details of the signal processing chain
- G01S19/36—Constructional details or hardware or software details of the signal processing chain relating to the receiver frond end
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04K—SECRET COMMUNICATION; JAMMING OF COMMUNICATION
- H04K3/00—Jamming of communication; Counter-measures
- H04K3/80—Jamming or countermeasure characterized by its function
- H04K3/90—Jamming or countermeasure characterized by its function related to allowing or preventing navigation or positioning, e.g. GPS
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04K—SECRET COMMUNICATION; JAMMING OF COMMUNICATION
- H04K2203/00—Jamming of communication; Countermeasures
- H04K2203/10—Jamming or countermeasure used for a particular application
- H04K2203/22—Jamming or countermeasure used for a particular application for communication related to vehicles
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04K—SECRET COMMUNICATION; JAMMING OF COMMUNICATION
- H04K2203/00—Jamming of communication; Countermeasures
- H04K2203/30—Jamming or countermeasure characterized by the infrastructure components
- H04K2203/32—Jamming or countermeasure characterized by the infrastructure components including a particular configuration of antennas
Abstract
Description
Claims
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE60324841T DE60324841D1 (en) | 2003-01-03 | 2003-12-17 | DOUBLE TRANSUNDANT GPS ANTISTOR AIRCRAFT NAVIGATION SYSTEM |
AU2003297413A AU2003297413B2 (en) | 2003-01-03 | 2003-12-17 | Dual redundant GPS anti-jam air vehicle navigation system |
BR0317932-0A BR0317932A (en) | 2003-01-03 | 2003-12-17 | Airborne navigation system with dual redundant gps anti-lock device |
EP03815230A EP1579233B1 (en) | 2003-01-03 | 2003-12-17 | Dual redundant gps anti-jam air vehicle navigation system |
CA002510147A CA2510147A1 (en) | 2003-01-03 | 2003-12-17 | Dual redundant gps anti-jam air vehicle navigation system |
JP2004566578A JP4425800B2 (en) | 2003-01-03 | 2003-12-17 | Aircraft navigation system using double redundant GPS to prevent interference |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10/336,553 US6710739B1 (en) | 2003-01-03 | 2003-01-03 | Dual redundant GPS anti-jam air vehicle navigation system architecture and method |
US10/336,553 | 2003-01-03 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2004063762A1 true WO2004063762A1 (en) | 2004-07-29 |
Family
ID=31978112
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US2003/040659 WO2004063762A1 (en) | 2003-01-03 | 2003-12-17 | Dual redundant gps anti-jam air vehicle navigation system |
Country Status (13)
Country | Link |
---|---|
US (1) | US6710739B1 (en) |
EP (1) | EP1579233B1 (en) |
JP (1) | JP4425800B2 (en) |
KR (1) | KR20050092034A (en) |
CN (1) | CN1735816A (en) |
AT (1) | ATE414913T1 (en) |
AU (1) | AU2003297413B2 (en) |
BR (1) | BR0317932A (en) |
CA (1) | CA2510147A1 (en) |
DE (1) | DE60324841D1 (en) |
ES (1) | ES2316875T3 (en) |
RU (1) | RU2336537C2 (en) |
WO (1) | WO2004063762A1 (en) |
Cited By (1)
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CN100382040C (en) * | 2006-10-24 | 2008-04-16 | 北京航空航天大学 | Redundant method for micro aircraft GNC system |
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JP2005043120A (en) * | 2003-07-24 | 2005-02-17 | Honda Motor Co Ltd | Navigation system for vehicle |
US7822105B2 (en) * | 2003-09-02 | 2010-10-26 | Sirf Technology, Inc. | Cross-correlation removal of carrier wave jamming signals |
JP4658050B2 (en) | 2003-09-02 | 2011-03-23 | サーフ テクノロジー インコーポレイテッド | Signal processing system for satellite positioning signals |
CN1975458B (en) * | 2006-12-12 | 2011-03-23 | 深圳市赛格导航科技股份有限公司 | Redundant GPS system and method thereof |
FR2947342B1 (en) * | 2009-06-30 | 2012-05-25 | Thales Sa | METHOD FOR DETERMINING THE POSITION OF A MOBILE TO A MOMENTUM AND MONITORING THE INTEGRITY OF THE POSITION OF THE MOBILE |
US9806790B2 (en) | 2010-03-29 | 2017-10-31 | Odyssey Wireless, Inc. | Systems/methods of spectrally efficient communications |
CN102207549A (en) * | 2010-05-05 | 2011-10-05 | 北京泰豪联星技术有限公司 | Integrated anti-interference satellite navigation receiving system and anti-interference processing method thereof |
RU2444752C1 (en) * | 2010-08-04 | 2012-03-10 | Открытое акционерное общество "Российская корпорация ракетно-космического приборостроения и информационных систем" (ОАО "Российские космические системы" | Assessment system of interference immunity of navigation circuit of artificial earth satellite (aes) |
CN103190076A (en) | 2010-08-30 | 2013-07-03 | 物理设备有限责任公司 | Tunable filter devices and methods |
US9042857B2 (en) | 2010-08-30 | 2015-05-26 | Physical Devices, Llc | Methods, systems, and non-transitory computer readable media for wideband frequency and bandwidth tunable filtering |
US8666347B2 (en) | 2010-10-14 | 2014-03-04 | Physical Devices, Llc | Methods and devices for reducing radio frequency interference |
US8594662B2 (en) * | 2011-02-03 | 2013-11-26 | Northrop Grumman Systems Corporation | Method and apparatus for protected communications to high altitude aircraft |
US9519062B2 (en) | 2012-02-28 | 2016-12-13 | Physical Devices, Llc | Methods, systems, and computer readable media for mitigation of in-band interference of global positioning system (GPS) signals |
US20130222180A1 (en) * | 2012-02-29 | 2013-08-29 | Gregory Thane Wyler | System and Method for Measuring Signal Power |
GB201311571D0 (en) * | 2013-06-27 | 2013-08-14 | Qinetiq Ltd | Signal processing |
US20150244431A1 (en) | 2014-02-21 | 2015-08-27 | Physical Devices, Llc | Devices and methods for diversity signal enhancement and cosite cancellation |
ES2699736T3 (en) * | 2014-04-04 | 2019-02-12 | Eutelsat Sa | Device and method to neutralize the impact of an interference signal on a satellite |
RU2558699C1 (en) * | 2014-05-22 | 2015-08-10 | ЗАО "ВНИИРА-Навигатор" | Complex method of aircraft navigation |
EP3254404A4 (en) | 2015-03-31 | 2018-12-05 | SZ DJI Technology Co., Ltd. | Authentication systems and methods for generating flight regulations |
JP6459014B2 (en) | 2015-03-31 | 2019-01-30 | エスゼット ディージェイアイ テクノロジー カンパニー リミテッドSz Dji Technology Co.,Ltd | Geo-fencing device |
CN113345271B (en) * | 2015-03-31 | 2022-12-27 | 深圳市大疆创新科技有限公司 | Method for detecting flight deviation of unmanned aerial vehicle |
RU2650582C1 (en) * | 2016-12-30 | 2018-04-16 | Акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" | Satellite navigation system of the winged rocket (options) |
CN107748376B (en) * | 2017-09-26 | 2021-02-02 | 南京航空航天大学 | Self-adaptive bandwidth tracking loop design method for satellite positioning receiver of unmanned vehicle |
JP6691096B2 (en) | 2017-12-11 | 2020-04-28 | 株式会社Subaru | Deception signal detection system and deception signal detection method |
JP6674437B2 (en) * | 2017-12-26 | 2020-04-01 | 株式会社Subaru | Auxiliary device for rotor, rotor, gas turbine engine and aircraft |
US11150671B2 (en) * | 2019-05-07 | 2021-10-19 | Qatar Foundation For Education, Science And Community Development | Method and system for jamming localization and supporting navigation system |
US11320528B1 (en) | 2019-11-20 | 2022-05-03 | Telephonics Corporation | Monopulse secondary surveillance radar system |
US11698461B1 (en) | 2019-11-20 | 2023-07-11 | Telephonics Corp. | GPS denial detection and reporting and mitigation |
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US6331835B1 (en) * | 1999-02-02 | 2001-12-18 | The Charles Stark Draper Laboratory, Inc. | Deeply-integrated adaptive GPS-based navigator with extended-range code tracking |
US6377892B1 (en) * | 2000-05-02 | 2002-04-23 | Rockwell Collins, Inc. | Integrated navigation system |
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2003
- 2003-01-03 US US10/336,553 patent/US6710739B1/en not_active Expired - Lifetime
- 2003-12-17 AU AU2003297413A patent/AU2003297413B2/en not_active Ceased
- 2003-12-17 CA CA002510147A patent/CA2510147A1/en not_active Abandoned
- 2003-12-17 EP EP03815230A patent/EP1579233B1/en not_active Expired - Lifetime
- 2003-12-17 ES ES03815230T patent/ES2316875T3/en not_active Expired - Lifetime
- 2003-12-17 CN CNA2003801081699A patent/CN1735816A/en active Pending
- 2003-12-17 BR BR0317932-0A patent/BR0317932A/en not_active IP Right Cessation
- 2003-12-17 DE DE60324841T patent/DE60324841D1/en not_active Expired - Lifetime
- 2003-12-17 RU RU2005124678/09A patent/RU2336537C2/en active
- 2003-12-17 AT AT03815230T patent/ATE414913T1/en not_active IP Right Cessation
- 2003-12-17 JP JP2004566578A patent/JP4425800B2/en not_active Expired - Lifetime
- 2003-12-17 KR KR1020057012491A patent/KR20050092034A/en not_active Application Discontinuation
- 2003-12-17 WO PCT/US2003/040659 patent/WO2004063762A1/en active Application Filing
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN100382040C (en) * | 2006-10-24 | 2008-04-16 | 北京航空航天大学 | Redundant method for micro aircraft GNC system |
Also Published As
Publication number | Publication date |
---|---|
CA2510147A1 (en) | 2004-07-29 |
RU2336537C2 (en) | 2008-10-20 |
AU2003297413A1 (en) | 2004-08-10 |
EP1579233A1 (en) | 2005-09-28 |
RU2005124678A (en) | 2006-01-20 |
US6710739B1 (en) | 2004-03-23 |
JP4425800B2 (en) | 2010-03-03 |
EP1579233B1 (en) | 2008-11-19 |
BR0317932A (en) | 2005-11-29 |
AU2003297413B2 (en) | 2008-04-03 |
JP2006513084A (en) | 2006-04-20 |
CN1735816A (en) | 2006-02-15 |
KR20050092034A (en) | 2005-09-16 |
DE60324841D1 (en) | 2009-01-02 |
ATE414913T1 (en) | 2008-12-15 |
ES2316875T3 (en) | 2009-04-16 |
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