RU2003124130A - METHOD FOR MONITORING OPERATIONAL CAPABILITY OF ON-BOARD RECEIVER-INDICATOR OF A SATELLITE RADIO NAVIGATION SYSTEM - Google Patents

METHOD FOR MONITORING OPERATIONAL CAPABILITY OF ON-BOARD RECEIVER-INDICATOR OF A SATELLITE RADIO NAVIGATION SYSTEM Download PDF

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Publication number
RU2003124130A
RU2003124130A RU2003124130/09A RU2003124130A RU2003124130A RU 2003124130 A RU2003124130 A RU 2003124130A RU 2003124130/09 A RU2003124130/09 A RU 2003124130/09A RU 2003124130 A RU2003124130 A RU 2003124130A RU 2003124130 A RU2003124130 A RU 2003124130A
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RU
Russia
Prior art keywords
indicator
navigation system
satellite radio
height
receiver
Prior art date
Application number
RU2003124130/09A
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Russian (ru)
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RU2254591C2 (en
Inventor
Владимир Михайлович Жуков (RU)
Владимир Михайлович Жуков
Михаил Владимирович Жуков (RU)
Михаил Владимирович Жуков
Original Assignee
ОАО "Уральское проектно-конструкторское бюро "Деталь" (RU)
ОАО "Уральское проектно-конструкторское бюро "Деталь"
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Application filed by ОАО "Уральское проектно-конструкторское бюро "Деталь" (RU), ОАО "Уральское проектно-конструкторское бюро "Деталь" filed Critical ОАО "Уральское проектно-конструкторское бюро "Деталь" (RU)
Priority to RU2003124130/09A priority Critical patent/RU2254591C2/en
Publication of RU2003124130A publication Critical patent/RU2003124130A/en
Application granted granted Critical
Publication of RU2254591C2 publication Critical patent/RU2254591C2/en

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  • Position Fixing By Use Of Radio Waves (AREA)
  • Navigation (AREA)

Claims (1)

Способ контроля работоспособности бортового приемоиндикатора спутниковой радионавигационной системы, заключающийся в сравнении выдаваемой приемоиндикатором информации об одной из координат с аналогичной информацией, полученной с помощью одной из навигационных систем, отличающийся тем, что измеряют высоту Нрв полета летательного аппарата с помощью установленного на нем радиовысотомера, определяют высоту hp местности, над которой находится летательный аппарат в момент измерения высоты, используя для этой цели данные о плановых координатах с выхода приемоиндикатора спутниковой радионавигационной системы и цифровую карту местности, вычисляют абсолютную высоту Нарв+hp, сравнивают ее с высотой Нпи, снимаемой с выхода приемоиндикатора спутниковой радионавигационной системы и формируют сигнал его работоспособности, если |Напи| меньше устанавливаемого порога П.A method for controlling efficiency onboard receiver-indicator of satellite radio navigation systems comprising comparing issued Radio information on one of the coordinates with similar information obtained via a navigation system, characterized in that the measured height H pB flight of the aircraft using the installed thereon altimeter determine the height h p of the terrain above which the aircraft is located at the time of height measurement, using for this purpose data on planned coordinates dyat from the output of the receiver-indicator of the satellite radio navigation system and a digital map of the area, calculate the absolute height H a = H pb + h p , compare it with the height H pi taken from the output of the receiver-indicator of the satellite radio-navigation system and form a signal of its operability if | Н а- Н pi | less than the set threshold P.
RU2003124130/09A 2003-07-31 2003-07-31 Mode of controlling working capacity of airborne receiver indicator of satellite radio navigational system RU2254591C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2003124130/09A RU2254591C2 (en) 2003-07-31 2003-07-31 Mode of controlling working capacity of airborne receiver indicator of satellite radio navigational system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2003124130/09A RU2254591C2 (en) 2003-07-31 2003-07-31 Mode of controlling working capacity of airborne receiver indicator of satellite radio navigational system

Publications (2)

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RU2003124130A true RU2003124130A (en) 2005-01-27
RU2254591C2 RU2254591C2 (en) 2005-06-20

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RU (1) RU2254591C2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112068087A (en) * 2020-10-17 2020-12-11 中国电波传播研究所(中国电子科技集团公司第二十二研究所) Shore-based multi-channel radar aircraft-simulated sea clutter measurement method

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112068087A (en) * 2020-10-17 2020-12-11 中国电波传播研究所(中国电子科技集团公司第二十二研究所) Shore-based multi-channel radar aircraft-simulated sea clutter measurement method
CN112068087B (en) * 2020-10-17 2022-03-01 中国电波传播研究所(中国电子科技集团公司第二十二研究所) Shore-based multi-channel radar aircraft-simulated sea clutter measurement method

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Publication number Publication date
RU2254591C2 (en) 2005-06-20

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Effective date: 20080801