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上海天文台 Shanghai Astronomical Observatory 4th IVS General Meeting Spacecraft Tracking with Chinese VLBI Network Xiuzhong Zhang and Chinese VLBI Network Team Shanghai Astronomical Observatory Chinese Academy of Sciences
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上海天文台 Shanghai Astronomical Observatory Outline 1. introduction 2. Configuration of tracking test system 3. Some test observation results 4. Plan of VLBI spacecraft tracking in China
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上海天文台 Shanghai Astronomical Observatory VLBI system with highest resolution technique is used for astronomers in radio wave domain; e-VLBI has got rapid progress in the past 4-5 years; More and more computing power with a single IC chip; With these characteristics, VLBI system becomes to possible to make real time tracking for spacecraft orbiting application. 1. Introduction
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上海天文台 Shanghai Astronomical Observatory Some events of spacecraft tracking with VLBI 1980s: VLA as a supersensitive deep space “ downlink ” station 1980s: NASA DSN stations (Goldstone, Robledo, Tidbinbilla) begin their VLBI duties 1984-86: VLBI tracking of the Venus baloons (VEGA mission) and VEGA-Giotto Pathfinder experiment (Intercosmos-ESA-NASA) 1990s: phase-referencing “ satellite-3C279 ” demo (Asaki, Sasao et al.) Activities of Spacecraft tracking with VLBI in Japan 2005: Radio Astronomy segment of the Huygens mission
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上海天文台 Shanghai Astronomical Observatory Huygens the Titan Probe as seen with a VLBI magnifier Leonid Gurvits and VLBI tracking team Joint Institute for VLBI in Europe (JIVE) Dwingeloo, The Netherlands
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上海天文台 Shanghai Astronomical Observatory Huygens VLBI tracking team (abbreviated) JIVEESA-ESTECNASA-JPLNRAO I.M.AvruchC.. van’t KloosterS.AsmarW.Brisken H.BignallJ.-P.LebretonW.FolknerF.Ghigo A.Brunthaler R.A.PrestonG.Langston R.M.Campbell J.Romney M.A.Garrett L.I.Gurvits, R.Oerlemans S.V.Pogrebenko ASTRONATNFU TasmaniaNICT (CRL) A.R.FoleyJ.Lovell G.Cimo T.Kondo C.Phillips. S.Elingsen U Bonn J. Reynolds B.Reid M.Bird R.Sault. T.Tzioumis NAO ChinaHelsinki UISAS T.An (ShAO)A.MujunenR.Dodson X.Hong(ShAO)J.Ritakari S.Huang(ShAO) D.Jiang(ShAO) X.Liu(UAO) 12 institutes and international organizations in 7 countries
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上海天文台 Shanghai Astronomical Observatory Spacecraft TT&C Signal Characteristics Narrow bandwidth several hundred KHz Relative strong signal to noise rate Special signal spectrum with special structure The dynamic range of signal amplitude relative large
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上海天文台 Shanghai Astronomical Observatory CVN started spacecraft tracking science 2001 Different orbit spacecraft have been observed with VLBI system. i.e. GEO, TC-1, TC-2, SMART-1, deep space probe VLBI tracking of the Venus balloon Many system equipment have been improved Prepare to do the orbiting of CE-1 Study of spacecraft tracking method Spacecraft tracking with VLBI in China
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上海天文台 Shanghai Astronomical Observatory VLBI Stations in China
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上海天文台 Shanghai Astronomical Observatory Nanshan (Urumqi) at sunrise Seshan (Shanghai)
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上海天文台 Shanghai Astronomical Observatory Beijing & Kunming station in constraction
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上海天文台 Shanghai Astronomical Observatory Test bed for receiver noise test
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上海天文台 Shanghai Astronomical Observatory 工艺设备 —— 上海测站子系统(天线改造后) Up: New S band feedback Left : New S/X band feedback
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上海天文台 Shanghai Astronomical Observatory New Antenna service system in Seshan station
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上海天文台 Shanghai Astronomical Observatory New S/X band Cryogenic Receivers in Seshan Station
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上海天文台 Shanghai Astronomical Observatory New S/X band Cryogenic Receivers in Nanshan Station
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上海天文台 Shanghai Astronomical Observatory New Pcal in Nanshan Station
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上海天文台 Shanghai Astronomical Observatory 5 Station Correlator in developing
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上海天文台 Shanghai Astronomical Observatory 3. Some test observation results
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上海天文台 Shanghai Astronomical Observatory Test Observations in March 17 – 20, 2005 SH(25m), UR(25m), KM(3m telescope) CVN Disk Array recorder S Band for TC-1, S/X Band for Radio Source 8 MHz Bandwidth for TC-1 and Radio Source Radio Source : 3C454.3 , 3C84 for correct the difference of station clocks
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上海天文台 Shanghai Astronomical Observatory Test observations in Mar. 17 – 20, 2005 with TC-1 Apogee : > 80000Km
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上海天文台 Shanghai Astronomical Observatory Orbiting result with VLBI Resuduals delay: 1.5624m(mean), 12.4448m(RMS)
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上海天文台 Shanghai Astronomical Observatory SMART-1 TT&C downlink signal Right Above : sheshan station Right Down : Urumqi station
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上海天文台 Shanghai Astronomical Observatory
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上海天文台 Shanghai Astronomical Observatory Observation of Smart-1 (SH – UR) Sept. 22, 2004 UTC, the distance between Smart-1 and the earth is more than 280,000Km. Used 0.5 second data via FTP for fringe checking, with these data, the delay accuracy is 0.6ns and delay rate accuracy is 1.8ps/s.
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上海天文台 Shanghai Astronomical Observatory Smart-1 orbiting with VLBI Observation Observe time (UT) : March 20, 2005 10 h 30 m 16 h 50 m Orbit of Smart-1 : polar orbit, apogee 2833Km , perigee 498Km , period 4.95 hours station : Seshan ( 25m ), Nanshan ( 25m ), Kunming ( 3m )。 Frequetion of carrie wave : 2235.10 MHz Observe frequency : 2230.99 2238.99 MHz Bandwidth : 8.0 MHz 。 Radio source : 3C84 , 4C39.25 , 3C279 。 MK5A recorder, 16 Mbps , Data processing : Shanghai VLBI data processing center Integration time : 4s
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上海天文台 Shanghai Astronomical Observatory Smart-1 S Band (2.2GHz) downlink Signal dB MHz Wide Band mode Narrow Band mode
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上海天文台 Shanghai Astronomical Observatory The compare results of delay and delay rate between VLBI observe and ESA Smart-1 reconstruction orbit Resuduals DelayResuduals delay rate SH - UR KM - SH KM - UR SH - UR KM - SH KM - UR
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上海天文台 Shanghai Astronomical Observatory Future Plans Develop and create a 4 stations VLBI network for astronomy and spacecraft tracking Prepare to do the near real time orbit tracking of CE-1 (Chinese lunar project, will be launched in 2007) Study the method of Deep space spacecraft tracking
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上海天文台 Shanghai Astronomical Observatory Thanks !
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