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CVN software correlator development and its applications Zheng Weimin*, Zhang Juan, Tong Li, Tong Fengxian, Liu Lei, Chen Zhong, Shu Fengchun, Wang Guangli.

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Presentation on theme: "CVN software correlator development and its applications Zheng Weimin*, Zhang Juan, Tong Li, Tong Fengxian, Liu Lei, Chen Zhong, Shu Fengchun, Wang Guangli."— Presentation transcript:

1 CVN software correlator development and its applications Zheng Weimin*, Zhang Juan, Tong Li, Tong Fengxian, Liu Lei, Chen Zhong, Shu Fengchun, Wang Guangli Shanghai Astronomical Observatory, Chinese Academy of Sciences 8th East Asia VLBI workshop, Sapporo, Japan 8 - 10 July, 2015 1

2 Outline 1.Development history 2.Applications in CE-3 mission 3.Development status 4.Future work 2 CVN software correlator

3 1. Development history 2003-2004 First CVN software correlator: Satellite Fringe searcher Matlab First domestic Geostationary, Elliptical Orbit Satellites VLBI correlation 2004-2007 FX type software correlator for Chinese Lunar Exploration Project (CE-1) c language ESA SMART-1, TC-1, TC-2 VLBI tracking experiment Hardware correlator debugger & backup in CE-1 preparation stage SMP parallelization 3CVN software correlator

4 2007-2010 Primary CVN correlator in CE-1, CE-2 lunar projects Near real time correlator, with satellite fringe search ability Data latency < 2min VLBI center latency ~ 6min 2011-2015 Primary correlator in CE-3, CE-5T1 projects Real time correlation & satellite fringe search ability MPI + OpenMP parallelization Data latency < 10sec VLBI center latency < 40sec 2011-2013 CVN Geodesy application of Crustal Movement Observation Network of China (CMONOC ) 4CVN software correlator

5 Outline 1.Development history 2.Applications in CE-3 mission 3.Development status 4.The future work 5 CVN software correlator

6 CE-3 Mission objective:  Complete the Chinese first soft-landing and roving exploration on the Moon (first probe to soft-land on the Moon since Luna 24 in 1976)  Demonstrate and develop key technologies for future missions.  Scientific objectives: Lunar surface topography, lunar surface material composition and resource survey, lunar-based astronomical observation, etc. 6 2. Applications in CE-3 mission

7 New Requirements & techniques of CVN 1.High accuracy 2.Real time ability 3.Accurate Moon surface positioning 4.Combined orbit determination ( X band ΔDOR ) DOR – Differential of One-way Range ( e-VLBI + real time data process pipleline) (Same Beam VLBI, SBI ) (2-way/ 3-way range + VLBI) 7

8 Mission Requirements on VLBI 1.Earth-Moon transfer orbit phase & circumlunar phase  ΔDOR tracking group delay < 4ns (Actuality <0.5ns)  Orbit & angular determination and orbit prediction ；  System data processing latency < 1minute (Actuality 15~40 seconds) 2.Lunar surface working phase  Lander & Rover tracking by SBI  Lander 3D position <1km (Actuality <100m )  Rover relative position of the lander <500m (Actuality ~1m ) 8

9 CVN data center real-time pipelines in CE-3

10 Block diagram software correlator NFS: Network File System

11 Computing platform Standard Linux cluster Five I/O nodes - E7-4820*4/ 128GB/ 300GB+12TB 32 compute nodes*12 cores fringe search + correlation - E5-2640*2/ 32GB/ 300GB 2 manage nodes - E5-2620*2/ 24GB/ 900GB+214GB Management network - 10G Ethernet Compute network - InfiniBand 11

12 Specifications of CE-3 software correlator 12 Processing ModeReal-time & post-processing Station number1~20 Real-time fast fringe search4 stations IF number1,2,4,8,16 Frequency channel24~16384/IF Integration period0.1~60 second Maximum data speed (192 CPU cores) About 1.9Gbps/station, totally 4 stations Output formatCVN, FITS-IDI

13 13 Rover positioning by same-beam VLBI 1.Differenced VLBI group delay Real time mode 2.Same beam phase reference image postprocess mode 3.Differenced VLBI phase delay, postprocess

14 Null test by same beam phase reference image positioning Local coordinateNorthEastDownDistance Same-beam phase- referencing VLBI result 1.197-0.005-0.7591.417 True value1.016-0.605-0.7591.405 Differences0.1810.6000.0000.012 Null test error: ~ 0.6 m

15 Rover A B C D E E17 15

16 Outline 1.Development history 2.Applications in CE-3 mission 3.Development status 4.The future work 16 CVN software correlator

17 3. Development status Increase correlation speed by MPI+Pthreads 6 stations * 1.1Gbps/station->2.0Gbps/station 192 CPU cores GPU acceleration: VGOS application Geodesy application: Output format CVN--> Mk4, Pulsar gate : Pulsar processing 17CVN software correlator

18 Via DiFX software package – cvn2difx: developed by our group – difx2mark4: provided by DiFX Direct convert – cvn2mark4: under development CVN visibility output delay model cvn2difx DiFX SWIN format.im file.input,.calc,.flag difx2mark4 Mark4 format type-0 (root) type-1 (corel) type-3 (station).vex vex2difx CVN visibility output delay model cvn2mark4 Mark4 format type-0 (root) type-1 (corel) type-3 (station).vex CVN to Mark4 format transform test

19 CVNDiFX

20 DiFX vs. CVN SC

21 Two GPU Nodes Each node:1 x Nvidia K40c GPU Workstation DELL T5600 ChipsetIntel C600 CPUIntel E5-2600 @ 2.00GHz Memory 64GB Ethernet Intel 82579 1Gb NIC InfinibandMellonax ConnectX 40Gb/s QDR GPUNVIDIA Kepler K40c GPU acceleration correlator prototype

22 CE-3 DOR delay difference: GPU SC vs. CPU SC GPU Speed/station 1 node 337Mbps 2 nodes670Mbps Four station speed test NVIDA K40C

23 20s integration without pulsar gate and dispersion correction Pulsar B0329+54 preliminary result 20s integration with pulsar gate and dispersion correction

24 4. Future work CVN needs a general purpose software correlator: Lunar and deep space exploration mission Geodesy and astronomy data processing Pulsar binning, multi-phase center ability VGOS broadband ability New software correlator CVN, IVS(VGOS), EVAN, AOV CVN software correlator24

25 Thank you for your attention!

26 Rover position （ 4 ways ） Site Visual+ Inertial navigation VLBI group delay VLBI phase delay VLBI phase reference map A N9.03-4.2 11.25 9.47 E1.55.41.28 1.15 B N5.00-269.8 5.89 5.12 E8.90-640.87.56 9.30 C N-5.6580.5 -4.92 -5.34 E8.3610.0 8.02 8.86 D N-9.75112.6 -8.73 -9.51 E0.2769.2 0.37 0.49 E N-19.7759.0 -17.35m -19.26 E-0.2032.0 -0.42 -0.29 E17 N-11.83/ / -11.063 E-13.05/ / -12.961

27 Residual statistics  VLBI group delay residuals ： ~ 1ns in trans-lunar orbit ~ 0.5ns in lunar orbit.

28 The Software Correlator Status of CVNSlide#: 28 Fast fringe search is closed! Fast fringe search is opened! The result of CVN software correlator using the fast fringe search function. The show tool is real-time monitoring tool developed by ourselves.

29 Perilune braking real time fringe search result

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