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 stationInfo
- 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
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.
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)
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 |
-
2010
- 2010-09-10 UA UAU201010907U patent/UA60974U/en unknown
Cited By (2)
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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