Äîêóìåíò âçÿò èç êýøà ïîèñêîâîé ìàøèíû. Àäðåñ îðèãèíàëüíîãî äîêóìåíòà : http://www.ipa.nw.ru/conference/wpltn2012/docs/24/1100%20shargorodsk.pdf Äàòà èçìåíåíèÿ: Mon Oct 1 12:08:08 2012 Äàòà èíäåêñèðîâàíèÿ: Sun Feb 3 20:33:05 2013 Êîäèðîâêà: Ïîèñêîâûå ñëîâà: ngc 6992

LASER GLONASS
Dr. Shargorodskiy Victor, dr. Kosenko Victor, dr. Chubykin Alexey, dr. Pasynkov Vladimir, dr. Sadovnikov Mikhail
Open Joint-stock Company «Research-and-Production Corporation «Precision Systems and Instruments» Reshetnev company 4 TCNII


LASER GLONASS
The biggest contribution in the balance of errors of GNSS user position determination is the error of the space segment consisting of navigation S/C constellation and S/C ground control system.

"Laser GLONASS" is a combination of methods and technology that will radically reduce that error.

Development of laser systems utilizing break-through information and measurement technologies is foreseen in 2012-2020 to achieve high accuracy characteristics of the GLONASS.

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LASER GLONASS
Purpose of creation of laser technologies and systems Achievement of GLONASS target characteristics

Component of error of position and time determination due to the space segment real time ­ up to 0.6 m and 0.1* m (base values ­ 2.8 m and 1.0* m) in posterior mode ­ up to 0.03 m (base value 0.1 m) up to 1 ns (base value ­ 5 ns) calibration - up to 0,1 ns *
using additional systems

Obtaining measurement data to reduce: error of reference of Federal Geocentric Coordinate System (FGCS) to the center of gravity of the Earth ­ down to 0.01 m (base value ­ 0.5 m) FGCS error in GLONASS ­ down to 0 .0 2 (base value ­ 0.2 m)

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LASER GLONASS
Laser GLONASS systems

Onboard systems
Array of

Ground systems
Network of

ISLNCS

OOSLR

CCR

GOSLR

SLR
collocation

SVOEVP

ISLNCS - Inter Satellite Laser Navigation and Communication System OOSLR ­ On-board One-way SLR GOSLR ­ Ground One-way SLR CCR ­ Corner Cube Reflector SVOEVP - System for high-accuracy determination of ephemeris and time corrections GMS ­ GNSS Monitoring System (radio) VLBI ­ Very Long Baseline Interferometry

SLR GMS

SLR GMS, VLBI SLR GMS, VLBI DORIS 4


LASER GLONASS
ISLNCS is designed for high-accuracy inter-satellite one-way measurements of pseudo-range
for:
Retroreflector array (AC 108 2)

- repeated determination of deviation of a S/C time scale drift with subnanosecond accuracy at every orbit, - integrity check of navigation field; - provision for global coverage with placement of S/C time synching systems on Russian territory only. ISLNCS

ISLNCS and retroreflector array onboard satellite "GLONASS-M"

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LASER GLONASS
ISLNCS measurement tasks are solved using high-accuracy counter-measurements of pseudo range between "GLONASS" navigation satellites Measurement data exchange is done using laser signals with time-pulse modulation
Pseudo range differs from the range by difference between time scales multiplied by the speed of light. In case of counter-measurements, this value will be included in pseudo-range measurements with different signs. Half-sum of counter pseudo-ranges is true range, and their half-distance unambiguously determines the shift of time scales between two S/C.

ISLNCS flight model

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LASER GLONASS
Problems solved by on-way SLR:
- calibration of on-board and ground GMS equipment during in-flight operations; - synching remote ground clocks at accuracy levels not achievable by radio systems and mobile frequency standards
Central time scale Retroreflector array GLONASS-M S/C

On-board one-way SLR

Remote clock time scale

One-way range channel

Two-way range measurement channel

Schematics of synching of onboard time scale and ground time scale and transmission of time to a remote ground station using one-way SLR

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LASER GLONASS
Operating principle of the laser system for determination of difference between onboard and ground time scales
The method of determination of difference between onboard and ground time scales is based on comparison of one-way and two-way distances measured at sub-centimeter levels.

Half of a two-way range differs from the one-way pseudo range by shift between time scales multiplied by the speed of light. Determination of this shift is at the level of 10-10 s.

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LASER GLONASS
SLR Network

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LASER GLONASS
Problems solved by SLR network
- calibration of active radio systems during their flight operations with sub-centimeter accuracy; - obtaining SLR, VLBI and GMS collocation data to provide GLONASS system with high-accuracy coordinate reference frame to ensure required accuracy of transfer of Federal Geocentric Coordinate System (FGCS) by GLONASS system; - evaluation of errors of representation of FGCS by GLONASS navigation field by comparison of SLR coordinates obtained from laser measurements of LAGEOS satellites with SLR coordinates obtained from laser measurements of GLONASS satellites; - check accuracy of calculation of high-accuracy ephemeris and time correction information SVOEVP. 10


LASER GLONASS
SLR
Shelkovo (Moscow Region) Svetloe

Komsomolsk-On-Amur

Altai

Baikonur

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LASER GLONASS
System for high-accuracy determination of ephemeris and time corrections (SVOEVP) Provision of real-time GLONASS ETS · calculation of SD for NFAF
· models support · support of GCS GSD Calculation of highaccuracy posterior data for provision of global positioning

Solution of fundamental problems
· FGCS support · geodynamic data calculation

ETS ­ Ephemeris and Time Support FGCS ­ Federal Geocentric Coordinate System GCS ­ Ground Control System GSD ­ geodetic source data NF ­ navigation field NFAF ­ navigation frame accuracy factor PETI ­ posterior ephemeris and time Information RT ­ Real Time SD ­ source data UNE ­ user navigation equipment

Information · generalized
evaluations of NF accuracy · information bulletins

RT navigation support
· assisting technology · remote calibration of UNE in the course of operation

Navigation provision in posterior mode · PETI GLONASS (GPS)
· parameters of local models of stratosphere, ionosphere, etc. · positioning in relative mode

Support for navigation of dynamic users in FGCS

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LASER GLONASS
SLR measurements are used in SVOEVP GLONASS for solution of the following problems:
check of transmission of the parameters of the Federal Geocentric Coordinate System (FGCS) to end users by GLONASS navigation signals; calculation of reference parameters and check of correspondence of parameters of the Federal Geocentric Coordinate System (FGCS) to the international reference frame (ITRF); check of posterior ephemeris information (PEI) of the SVOEVP using comparison of two-way laser measurement of slant ranges with ranges obtained from PEI; check of posterior time and frequency information using comparison of two-way SLR range with one ­way range obtained by on-board one-way SLR (or GMS); use of SLR measurements for calculation of velocities of ground stations motion for refinement and support of initial geodetic data of GLONASS ground control system; refinement of location determination of phase centers of satellite antennae systems and analysis of spacecraft attitude system work quality using comparison of one-way SLR and GMS data; calculation of calibration corrections of GLONASS navigation equipment, evaluation of accuracy of user navigation equipment; calculation of calibration corrections and check of accuracy of two-way and one-way radio measurement systems; support of malfunctioning GLONASS satellites in the case of partial and complete failure of onboard radio systems, including daytime observations.

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LASER GLONASS
Conclusion:
Development of experimental and serial units of onboard and ground equipment is foreseen in the Federal Target Program "Support, development and operation of GLONASS system in 2012-2020. Creation of "Laser GLONASS" and, therefore, achievement of parity and, perhaps, superiority to the world level of potential accuracy of ephemeris and time support is a real deal in the near future.

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LASER GLONASS

Thank you for your attention!