UA60974U - Method for control of integrity of satellite navigation system in control-correction station - Google Patents

Method for control of integrity of satellite navigation system in control-correction station

Info

Publication number
UA60974U
UA60974U UAU201010907U UAU201010907U UA60974U UA 60974 U UA60974 U UA 60974U UA U201010907 U UAU201010907 U UA U201010907U UA U201010907 U UAU201010907 U UA U201010907U UA 60974 U UA60974 U UA 60974U
Authority
UA
Ukraine
Prior art keywords
navigation
control
quasi
coordinates
additional channels
Prior art date
Application number
UAU201010907U
Other languages
Russian (ru)
Ukrainian (uk)
Inventor
Валерий Викторович Конин
Эдуард Александрович Ковалевский
Александр Викторович Куценко
Original Assignee
Национальный Авиационный Университет
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 Национальный Авиационный Университет filed Critical Национальный Авиационный Университет
Priority to UAU201010907U priority Critical patent/UA60974U/en
Publication of UA60974U publication Critical patent/UA60974U/en

Links

Landscapes

  • Position Fixing By Use Of Radio Waves (AREA)

Abstract

Method for control of integrity of satellite navigation system in control-correction station includes measurement of radio-navigation parameters (quasi-distances) by signals from N navigation satellites (main channel), formation of combinations of massifs of quasi-distances with exclusion of massif of quasi-distance to i-th navigation satellite (additional channels), solution of navigation problem with determination of coordinates of user by main and additional channels, formation of test statistics as difference of coordinates determined and making decision on presence or absence of failure of navigation satellite through comparison to threshold. In each combination of massifs of quasi-distances in additional channels instead of quasi-distance to i-th navigation satellite included distance calculated by known coordinates of i-th navigation satellite and used is added, and test statistics is formed through averaging differences determined in main and additional channels of coordinates of user by several different measurements.
UAU201010907U 2010-09-10 2010-09-10 Method for control of integrity of satellite navigation system in control-correction station UA60974U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
UAU201010907U UA60974U (en) 2010-09-10 2010-09-10 Method for control of integrity of satellite navigation system in control-correction station

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
UAU201010907U UA60974U (en) 2010-09-10 2010-09-10 Method for control of integrity of satellite navigation system in control-correction station

Publications (1)

Publication Number Publication Date
UA60974U true UA60974U (en) 2011-06-25

Family

ID=50835148

Family Applications (1)

Application Number Title Priority Date Filing Date
UAU201010907U UA60974U (en) 2010-09-10 2010-09-10 Method for control of integrity of satellite navigation system in control-correction station

Country Status (1)

Country Link
UA (1) UA60974U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2585051C1 (en) * 2015-04-08 2016-05-27 Открытое акционерное общество Московский научно-производственный комплекс "Авионика" имени О.В. Успенского (ОАО МНПК "Авионика") Method of controlling data from satellite navigation systems and device therefor
CN110398975A (en) * 2019-09-04 2019-11-01 西北工业大学 A kind of navigator's follower type multiple aircraft formation fault tolerant control method based on broadcast operation framework

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2585051C1 (en) * 2015-04-08 2016-05-27 Открытое акционерное общество Московский научно-производственный комплекс "Авионика" имени О.В. Успенского (ОАО МНПК "Авионика") Method of controlling data from satellite navigation systems and device therefor
CN110398975A (en) * 2019-09-04 2019-11-01 西北工业大学 A kind of navigator's follower type multiple aircraft formation fault tolerant control method based on broadcast operation framework

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