Status, Development and Application



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Federal Space Agency GLONASS GLONASS Status, Development and Application Sergey G. Revnivykh International Committee on Global Navigation Satellite Systems (ICG) Second Meeting, September 4-7, 2007, Bangalore, India

Contents GLONASS State Policy GLONASS Architecture GLONASS Modernization Program International cooperation Summary

Federal Space Agency GLONASS GLONASS State Policy

GNSS Features GNSS become the global strategic utility used in many countries in the all areas of economy in many applications Presently the US GPS is widely in use. The Russian GLONASS has been fully deployed in 1995, now is in the reconstruction and development phase. The EU GALILEO is in progress to be deployed by 2012. GNSS systems are highly sensitive to interference and jumming There is a risk to provide the reliable navigation and economy development for many countries when only one system is applied To reduce the risk and to provide sustainable economy development: - Highly important to rely on two systems at least for redundancy GLONASS is a basis to reduce the risk and support sustainable development of economy

Basic principles of the GLONASS State Policy GLONASS is an element of the critical state infrastructure ensuring national security and development of economy GLONASS is a dual use system Access to civilian GLONASS service is free of direct user fee Documentation on the open GLONASS service is available for user community, developers and manufacturers of the navigation equipment Support development and production of the combined receivers GLONASS/GPS Providing compatibility and interoperability with others GNSS and augmentations (GPS, GALILEO ) Encouraging the navigation mass market development Binding use of GLONASS or GLONASS/GPS combine receivers to the state users

New Presidential Decree on GLONASS Issued at May 18, 2007 Main statements: Free access to the civil signals GLONASS binding use for governmental and strategic applications Recommended: GLONASS use for regional authorities and commercial companies General coordination of GLONASS sustainment, development and application Federal Space Agency To the Government: GLONASS promotion, including international cooperation Digital maps issue to be resolved asap Preparation of the new GLONASS Program for 2012 2020.

Federal GLONASS Program for 2002-2011 1 2 Subprograms GLONASS GLONASS sustainment, sustainment, development development and and deployment deployment User User equipment equipment development development for for civil civil users users 3 Satellite Satellite navigation navigation technique technique implementation implementation in in transport transport areas areas 4 Geodesy Geodesy reference reference improvement improvement 5 User User equipment equipment development development for for military military users users

Federal Space Agency GLONASS GLONASS Architecture

GLONASS architecture GLONASS System Orbital constellation Ground Control Segment Launchers and Launch Facilities User segment (State regulated) Glonass SC control PROTON Military Glonass-M Orbit determination SOYUZ Civil Glonass-K Time synchronization 9

GLONASS Orbits Orbit constellation: 24 satellites, 3 planes by 8 satellites Orbit shift by 120 along the equator Orbit parameters orbit circular height 19100 km inclination 64.8 revolution 11h15 15min

Constellation Status In orbit 17 satellites 7 7 new GLONASS-M 10 old GLONASS Healthy 10 sats In commissioning 1 sat In maintenance 1 sat In decommissioning 5 sats Launches in 2007: Block 36 (3 Glonass-M) Block 37 (3 Glonass-M)

Main Specifications Glonass-M spacecraft Guaranteed life time 7 years Spacecraft mass 1415 kg Power supply 1450 W Navigation payload Mass Power consumption Clock stability Attitude control accuracy Solar panel pointing accuracy 250 kg 580 W 1*10-13 0.5 deg 2 deg Main features Extended life time Second civil signal L2 Increased clock stability Better accuracy of the solar panel pointing Improved dynamic model

Navigation Payload Antenna, power amplifiers, secondary control units Signal generator specification: Frequency band L1, MHz 1600 L2, MHz 1250 Radiating power L1, W 64 L2, W 40 Data rate at L1 и L2, 50 Navigation signal generator 13

On-board Clock Stability: 1*10-13 Three atomic frequency generators Synchronization unit 14

Ground Control Segment MS Murmansk MS MS TT&C St.-Peterburg Vorkuta Yakutsk Krasnoznamensk SCC MS Zelenchuk Schelkovo MS TT&C ULS CC SLR Yenisseisk MS TT&C ULS Komsomolsk MS TT&C ULS CC SLR Ulan-Ude Ussuriysk MS Nurek TT&C MS MS

Launchers PROTON-K launcher with «DM» PROTON-K launcher with «DM» booster booster SOYUZ-2 launchers with FREGAT SOYUZ-2 launchers with FREGAT booster booster Baykonur Plesetsk 16

System of Differential Corrections and Monitoring (SDCM) wide area aurmentation Main Objectives: Orbit and clock correction transmission to users Integrity provision Status: Limited monitoring network deployed Operation tests Validation 2010

GLONASS/GPS boards and chip sets User equipment Individual navigation Aviation Maritime Geodesy Integrated information navigation systems User Equipment

Federal Space Agency GLONASS GLONASS-M Flight Test (not yet completed)

GLONASS-M SISRE (today status) Flight test results Main problem clock synchronization

Requirement: On-board clock stability (observed) 1*10-13 Achieved results: For all GLONASS-M (without Gl-M M # 13) < 1*10-13 GLONASS-M M # 17 2-4*10-14 Better than requirements 1E-11 1E-12 1E-13 1E-14 100 1*10-13 R06 R07 R10 R14 R23 R24 1000 1*10-13 10000 100000

Federal Space Agency GLONASS GLONASS Modernization

GLONASS Requirement Document Update Improved Accuracy (open service) SIS positioning and timing, all-in in-view, full constellation (95%) <1.6 horizontal <2.6 vertical <5 ns New civil signals L3PT FDMA L1CR and L5R interoperable with GPS and Galileo Improved geodesy reference PZ-90.XX wrt ITRF < 5 cm Improved time reference GloST wrt UTC (SU) <120 ns with accuracy 6 ns Approval has to be done by the end of 2007

GLONASS Accuracy Improvement Program positioning accuracy 30 25 20 25 м ГЛОНАСС СДКМ GPS 15 10 5 0 10.5 м 5 м 2.3 м 2.4 м 1.5 м 2007 (2 кв) 2007 (4 кв) 2009 2010-2011 Wide Area Augmentation Two-way technique for OD&TS Measurements: 5 TT&C stations Combine Two-way and One-way OD&TS technique Measuremets + 3 MS 1 ULS Geodesy reference update Full constellation of 24 satellites Extension of monitoring network Measurements ++ 6 MS 2 ULS On-board clock stability improvement to 5*10-14 Global MS network Measurements +++: 6-10 stations outside Russia

Signal Modernization -7 L2PT +9 1243 1250-7 1598 L1PT +9 1607 1217 1238 1255 1593 R/A 1176, 45 1612 GLONASS existing signals L5R (TBC) L3PT -7 +9 1202 1208-7 L2PT +9 1243 1250 L1СR (TBC) L1PT -7 +9 1598 1607 1217 1238 1255 1593 R/A 1176,45 1176, TBC 45 1197 1575,42 TBC 1612 GLONASS-K L1CR, L5R: pending final decision

PZ-90.02 Governmental Decision of 20 June 2007: PZ-90.02 implementation in GLONASS Further permanent improvement toward ITRF New geodesy reference in GLONASS To be introduced at 20 September 2007 PZ-90.02 coordination to ITRF: No rotation Delta X: Delta Y: Delta Z: -36 cm +8 cm +18 cm GLONASS orbit accuracy improvement by 15-25 %

GLONASS Development Program Continuous global navigation by 2010 24 satellites in constellation GLONASS performance to be comparable with GPS (2010) Ground control segment modernization Monitoring station network extension (Russia) System time scale improvement Monitoring network outside Russia Signal modernization Third civil signal at L3 (since GLONASS-K K in 2009-2010 2010) New interoperable signals at L1 (L1CR) and L5 (L5R) Interoperability with GPS and future GALILEO Geodesy system Time system Further modernization of GLONASS based on new GLONASS-KM satellite

Federal Space Agency GPS GLONASS Galileo International cooperation

Objective background for international cooperation GNSS become the global strategic utility for National security Economy development Necessity to coordinate activity between system providers during the system development and modernization Necessity to provide compatibility and interoperability to benefit users when the combine receivers are in use

Benefits of the combine use Improved availability in the city canyons Increase robustness in the interfering conditions Reliability of service

International Cooperation Principles Encouraging of GLONASS use all over the world to sustainable development Open access of all users to the civil signals free of direct user charge GLONASS compatibility and interoperability with other GNSS and augmentations (GPS, Galileo, WAAS, EGNOS, IRNSS/GAGAN, QZSS ) Ensure the interests of the Russian Federation having in mind the dual use status of GLONASS as an element of the strategic state infrastructure International cooperation concept is to be completed by the end of 2007

Priority direction of the International Cooperation in GNSS Radio frequency compatibility RNSS frequency band protection Interoperability with GPS and GALILEO and augmentations in sense of signals, geodesy reference and time reference Development of common standards for GNSS application GNSS service certification Advance SatNav technology development Search and rescue service implementation on GNSS Integrity monitoring

User Interface Information Analysis Center of Positionin, Navigation and Time support (division of the Central Research Institute of Roscosmos) Daily bulletins on GLONASS and GPS status based on global data GLONASS control center official information Monthly bulletin with detail analysis of system performance Navigation news GLONASS icd www.glonass-ianc.rsa.ru IAC PNT feed back in the GLONASS control loop

Federal Space Agency GLONASS Summary

Summary GLONASS system is an element of the critical state infrastructure, ensuring national security and economy development, remains being a dual use system Urgent GLONASS restoration, development and mass use is one of priorities of the Russian State policy GLONASS essential element of the international GNSS to secure sustainable development and economy growth

Federal Space Agency GLONASS Thank you for your attention!