GLONASS – RUSSIAN GLOBAL NAVIGATION
SATELLITE SYSTEM
INTRODUCTION
• GLONASS acronym for "Global Navigation Satellite System", is a space-based satellite
navigation system operated by the Russian Aerospace Defence Forces.
• It provides an alternative to Global Positioning System (GPS) and is the only
alternative navigational system in operation with global coverage and of comparable
precision.
• Development of GLONASS began in the Soviet Union in 1976.
• Glonass (a global navigation satellite system) is being built by Reshetnev Information
Satellite Systems and is based on the US global positioning system (GPS).
• It is currently being operated by the Russian Space Forces on behalf of the Russian
Government
DEVELOPMENT
• The Soviet Union recognized the need to develop a new satellite-based radio navigation system in
the 1970s.
• The development of the Glonass satellite system began in 1976 with the aim of achieving global
coverage by 1991.
• About 43 Glonass satellites, as well as five additional test satellites, were successfully launched
from 1982 to 1991.
• The Russian Federation took over the development of Glonass upon dissolution of the Soviet
Union in 1991.
• Glonass achieved full deployment in 1995, with 24 satellites positioned in three different orbital
planes.
• Russia was unable to maintain the system until 2001 due to a financial crisis, which resulted in
only eight spacecraft being operational.
COMMUNICATION
• The Glonass system transfers data to a ground control station (GCS)
using a standard precision (SP) signal and modified high precision
(HP) signal.
• Real-time data is transmitted to the GCS using a 15-channel
frequency division multiple access (FDMA) procedure.
• FDMA is a channel access technique which assigns different
frequencies to multiple users for communications.
• Swepos, the Swedish national network of permanent satellite
reference stations, is currently integrating Glonass into its
operations.
VARIATIONS
• The Glonass system satellites have three versions, namely Glonass, Glonass-M and Glonass-K.
• The Glonass was initially designed for a lifespan of 14 months but later this was extended up to
two years.
• The Glonass-M is an upgraded model which has a lifespan of seven years.
• It features 12 primary antennas for L-band transmissions and laser corner-cube reflectors for orbit
determination and geodetic research.
• Glonass-K is the latest version with a lifespan of ten to 12 years.
• The Glonass-K satellite completed thermal vacuum (TVAC) tests at the RISS facility in June 2010.
• The satellite is fitted with a precision thermal control system to maintain a temperature of 0.1°C.
• It completed acoustic tests in August 2010.
INCEPTION
• The first satellite-based radio navigation system developed in the Soviet Union was Tsiklon,
which had the purpose of providing ballistic missile submarines a method for accurate
positioning.
• 31 Tsiklon satellites were launched between 1967 and 1978.
• The main problem with the system was that, although highly accurate for stationary or slow-
moving ships, it required several hours of observation by the receiving station to fix a position,
making it unusable for many navigation purposes and for the guidance of the new generation of
ballistic missiles.
• In 1968–1969, a new navigation system, which would support not only the navy, but also the air,
land and space forces, was conceived.
• Formal requirements were completed in 1970; in 1976, the government made a decision to
launch development of the "Unified Space Navigation System GLONASS".
DESIGN
• The task of designing GLONASS was given to a group of young specialists at
NPO PM in the city of Krasnoyarsk-26.
• Under the leadership of Vladimir Cheremisin, they developed different
proposals, from which the institute's director Grigory Chernyavsky selected the
final one.
• The work was completed in the late 1970s; the system would consist of 24
satellites operating at an altitude of 20,000 km in medium circular orbit.
• It would be able to promptly fix the receiving station's position based on signals
from 4 satellites, and also reveal the object's speed and direction.
• The satellites would be launched 3 at a time on the heavy-lift Proton rocket.
REFERENCES
• http://www.insidegnss.com/auto/popupimage/GLONASS%20SDCM%20architecture.jpg
• http://www.glonass.it/images/glonass_network.jpg
• http://www.svetandroida.cz/media/2014/05/188269259.jpg
• http://www.navipedia.net/images/thumb/5/5d/GLONASS_SpaceSegmentModernization.J
PG/400px-GLONASS_SpaceSegmentModernization.JPG
• http://www.aerospace-technology.com/projects/glonasssatellites/glonasssatellites3.html
• http://en.wikipedia.org/wiki/GLONASS
• http://www.aerospace-technology.com/projects/glonasssatellites/
THANK YOU

Glonass

  • 1.
    GLONASS – RUSSIANGLOBAL NAVIGATION SATELLITE SYSTEM
  • 2.
    INTRODUCTION • GLONASS acronymfor "Global Navigation Satellite System", is a space-based satellite navigation system operated by the Russian Aerospace Defence Forces. • It provides an alternative to Global Positioning System (GPS) and is the only alternative navigational system in operation with global coverage and of comparable precision. • Development of GLONASS began in the Soviet Union in 1976. • Glonass (a global navigation satellite system) is being built by Reshetnev Information Satellite Systems and is based on the US global positioning system (GPS). • It is currently being operated by the Russian Space Forces on behalf of the Russian Government
  • 4.
    DEVELOPMENT • The SovietUnion recognized the need to develop a new satellite-based radio navigation system in the 1970s. • The development of the Glonass satellite system began in 1976 with the aim of achieving global coverage by 1991. • About 43 Glonass satellites, as well as five additional test satellites, were successfully launched from 1982 to 1991. • The Russian Federation took over the development of Glonass upon dissolution of the Soviet Union in 1991. • Glonass achieved full deployment in 1995, with 24 satellites positioned in three different orbital planes. • Russia was unable to maintain the system until 2001 due to a financial crisis, which resulted in only eight spacecraft being operational.
  • 6.
    COMMUNICATION • The Glonasssystem transfers data to a ground control station (GCS) using a standard precision (SP) signal and modified high precision (HP) signal. • Real-time data is transmitted to the GCS using a 15-channel frequency division multiple access (FDMA) procedure. • FDMA is a channel access technique which assigns different frequencies to multiple users for communications. • Swepos, the Swedish national network of permanent satellite reference stations, is currently integrating Glonass into its operations.
  • 7.
    VARIATIONS • The Glonasssystem satellites have three versions, namely Glonass, Glonass-M and Glonass-K. • The Glonass was initially designed for a lifespan of 14 months but later this was extended up to two years. • The Glonass-M is an upgraded model which has a lifespan of seven years. • It features 12 primary antennas for L-band transmissions and laser corner-cube reflectors for orbit determination and geodetic research. • Glonass-K is the latest version with a lifespan of ten to 12 years. • The Glonass-K satellite completed thermal vacuum (TVAC) tests at the RISS facility in June 2010. • The satellite is fitted with a precision thermal control system to maintain a temperature of 0.1°C. • It completed acoustic tests in August 2010.
  • 9.
    INCEPTION • The firstsatellite-based radio navigation system developed in the Soviet Union was Tsiklon, which had the purpose of providing ballistic missile submarines a method for accurate positioning. • 31 Tsiklon satellites were launched between 1967 and 1978. • The main problem with the system was that, although highly accurate for stationary or slow- moving ships, it required several hours of observation by the receiving station to fix a position, making it unusable for many navigation purposes and for the guidance of the new generation of ballistic missiles. • In 1968–1969, a new navigation system, which would support not only the navy, but also the air, land and space forces, was conceived. • Formal requirements were completed in 1970; in 1976, the government made a decision to launch development of the "Unified Space Navigation System GLONASS".
  • 11.
    DESIGN • The taskof designing GLONASS was given to a group of young specialists at NPO PM in the city of Krasnoyarsk-26. • Under the leadership of Vladimir Cheremisin, they developed different proposals, from which the institute's director Grigory Chernyavsky selected the final one. • The work was completed in the late 1970s; the system would consist of 24 satellites operating at an altitude of 20,000 km in medium circular orbit. • It would be able to promptly fix the receiving station's position based on signals from 4 satellites, and also reveal the object's speed and direction. • The satellites would be launched 3 at a time on the heavy-lift Proton rocket.
  • 13.
    REFERENCES • http://www.insidegnss.com/auto/popupimage/GLONASS%20SDCM%20architecture.jpg • http://www.glonass.it/images/glonass_network.jpg •http://www.svetandroida.cz/media/2014/05/188269259.jpg • http://www.navipedia.net/images/thumb/5/5d/GLONASS_SpaceSegmentModernization.J PG/400px-GLONASS_SpaceSegmentModernization.JPG • http://www.aerospace-technology.com/projects/glonasssatellites/glonasssatellites3.html • http://en.wikipedia.org/wiki/GLONASS • http://www.aerospace-technology.com/projects/glonasssatellites/
  • 14.