SVOM mission: ATF280F/AT697F data processing for real-time GRB detection and localization & ATF280E SpaceWire CEA IP recent developments

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1 SVOM mission: ATF280F/AT697F data processing for real-time GRB detection and localization & ATF280E SpaceWire CEA IP recent developments T.Chaminade, F.Château, F.Daly, M.Donati, C.Flouzat, P.Kestener, H.Le Provost, S.Schanne, P.Venault, M.Carty, L.Dumaye, J.Fontignie, D. Huynh, R.Joannes, T.Tourrette (UTS) F.Pinsard, C.Cara, J.A.Martin (SW) ESA, November CEA DSM Irfu SVOM UTS SEFUW 6-7 November 2012, ESA 1

2 SVOM: Instrument Gamma Ray Burst (GRB) trigger CXG (X/g camera) CdTe, kev photon timing 10 μs Franco-Chinese Instrument ITAR, EAR exportation rules constraints Real time GRB detection hardware based on ATMEL AT697F/ATF280F components 09/11/2012 CEA DSM Irfu SVOM UTS SEFUW 6-7 November 2012, ESA 2

3 On-board Gamma Ray Burst detection Gamma Ray Burst (GRB) Photon events Coded Mask Photon events (Pixel number, Hit time) Real time complex analysis: processor CXG camera 6400 Pixels UTS Detected GRB Logic device (FPGA) Interruption Processor Treatment Detected GRB Preprocessing & Formatting Shared memory Scientific Treatment Unit (UTS) 11/9/2012 CEA DSM Irfu SVOM UTS SEFUW 6-7 November 2012, ESA 3

4 UTS architecture Data Processing Model Virtex-4 IT Interruption every 10 ms PCI Bus Memory Bus Memory Shared Memory CXG photons FPGA ATF280F Processor AT697F Photon 1 Photon 2 Circular Photon Buffer Preprocessing & Formatting Treatment Formatting FPGA ATF280F Detected GRB sent via a SpaceWire link 1 PCI cycle 1 Memory cycle Additional FPGA preprocessing: raw data buffers, counting per pixel (Read/Modify/Write), per camera zone, per energy. Sophisticated DMA. 11/9/2012 CEA DSM Irfu SVOM UTS SEFUW 6-7 November 2012, ESA 4

5 UTS Data Processing Model Compact PCI Backplane XILINX V4 FPGA Board AT697F CPU Board PC (Host) Ethernet (TFTP ou NFS) -Config files -Result files Console (stdout) -print output Injector board Photon injection (CXG simulator) CPU monitor (grmon) -Load prog, run, status 11/9/2012 CEA DSM Irfu SVOM UTS SEFUW 6-7 November 2012, ESA 5

6 ATF280F firmware design flow UTS VHDL Design Xilinx wrapper for ATF280F I/O (bibufrr, obufer..) Synthesis, Xilinx P&R Full system test on Data Processing Model VHDL SIMULATION UTS VHDL Design Atmel wrapper for Xilinx FIFO, RAM modules Precision synthesis, IDS Atmel P&R Post routing ATF280F VHDL net list with Standard Delay File timing 11/9/2012 CEA DSM Irfu SVOM UTS SEFUW 6-7 November 2012, ESA 6

7 CXG Clock CXG Link 7 CXG Link 0 Photon preprocessing logic CPU Interrupt CXG Raw Data PCI Bus CXG Link Emulator 0 CXG Link Emulator 7 CXG Link Control 0 CXG Link Control 7 CXG Link Arbiter Raw Photons Buffer Interrupt Controller UTS Time Control Data Processing & Routing / AHB Master Access RAM Pointers AHB Bus AHB /PCI Bridge Modified Gaisler PCI_MT IP ATF280F FPGA Multiple Bus routing Distributed Memory usage (FIFO, RAM) UTS Control & Status Photon Counters 36x32-bit AHB Slave Access 11/9/2012 CEA DSM Irfu SVOM UTS SEFUW 6-7 November 2012, ESA 7

8 Photon preprocessing logic Resources ATF280F- MQFP352 XC4VLX100-10ff1513 ATFS450- MQFP352 I/O % % % FF % % % RAM 151 RAM Cells 17% 11 RAMB RAM16x1 logic 8753 core cells for routing 61% 15% 4337 LUTs for routing 4% 151 RAM Cells 10% 4% 0,2% 7866 for routing 34% 6% Performances Frequency 20 MHz* 63 MHz** 21 MHz* Atmel P&R tool: IDS 9.1.2a *- 55 C to +125 C ** 0 C to +85 C Only one global clock, PCI clock slowed down from 33 MHz to 20 MHz I/O registers for all external interfaces ATF280F 10% logic occupancy margin for future improvements 11/9/2012 CEA DSM Irfu SVOM UTS SEFUW 6-7 November 2012, ESA 8

9 UTS processor board CXG photons IT FPGA ATF280F Interruption every 10 ms PCI Bus Processor AT697F Laboratory Model Memory Bus Memory Photon 1 Photon 2 Shared Memory Circular Photon Buffer Preprocessing & Formatting Treatment Formatting FPGA ATF280F Detected GRB sent via a SpaceWire link Very similar to the engineering model mechanics, thermal, components 11/9/2012 CEA DSM Irfu SVOM UTS SEFUW 6-7 November 2012, ESA 9

10 UTS processor board (Laboratory Model) PCI-bus (ELS-FPGA board connector) Test board ATMEL FPGA 20 MHz application EEPROM 3D+ 4MB Leon2 CPU 100 MHz Max boot PROM 128 kb SDRAM 3D+ 512 MB LICE SpaceWire PPS 11/9/2012 CEA DSM Irfu SVOM UTS SEFUW 6-7 November 2012, ESA 10

11 UTS processor board (Laboratory Model) Functionalities - processor@66 MHz LEON2 processor (console, DSU monitor, program execution) SDRAM Boot EEPROM Application EEPROM FPGA ATF280F (loading*, VHDL code execution) *hotline ATMEL request pending for FPGA/AT17LV10 PROM compatibility State Isolate application EEPROM to allow SDRAM MHz SpaceWire firmware to be added 09/11/2012 CEA DSM Irfu SVOM UTS SEFUW 6-7 November 2012, ESA 11

12 UTS Design summary Full ATF280F firmware validated on the Data Processing Model tightly coupled to the AT697F RT GRB trigger software Precision/IDS tool suit stable and easy to use post routing simulation with modelsim SE works fine Major drawback of ATF280F is the final system frequency (penalties for Shadowgram RMW cycles in our application) no major upgrade with the ATFS450 09/11/2012 CEA DSM Irfu SVOM UTS SEFUW 6-7 November 2012, ESA 12

13 SpaceWireCEA IP Performance tests: configuration Hardware: Software: Aerospace Development Kit ATMEL (with ATF280E) PCI acquisition board - PCI4SpW VHDL synthesiser Precision RTL 2008a1.11 OEM_Atmel from MENTOR Place and Route Atmel Figaro IDS V9.0.2 Programming tool SpaceProgrammer Simulator ModelSim from MENTOR and the SpaceWireCEA IP 09/11/2012 CEA DSM Irfu SW IP SEFUW 6-7 November 2012, ESA 13

14 SpaceWireCEA IP: Footprint SpW IP config FIFO Size 9 x 32 Resource Used Utilization Combinational Cell 576 4% Sequential Cell % 11/9/2012 CEA DSM Irfu SW IP SEFUW 6-7 November 2012, ESA 14

15 SpaceWireCEA IP: performance Rx \ Tx 10 MHz * 30 MHz ** 50 MHz * 10 MHz 40 MHz 100 MHz Rx to Tx loop 120 MHz 140 MHz Rx \ Tx 10 MHz * 30 MHz ** 50 MHz * 10 MHz 40 MHz 100 MHz 120 MHz Frame generator 140 MHz * Global clock input - ** Fast Clock 09/11/2012 CEA DSM Irfu SW IP SEFUW 6-7 November 2012, ESA 15

16 SpaceWireCEA IP: effect of the temperature Rx to Tx loop with Tx=30MHz Rx freq -20 C 0 C +20 C +50 C 10 MHz Data Time-code 100 MHz Data Time-code 120 MHz Data Time-code 140 MHz Data Time-code Frame generator with Rx=100MHz Tx freq -20 C 0 C +20 C +50 C 30 MHz Data Time-code 50 MHz Data Time-code 11/9/2012 CEA DSM Irfu SW IP SEFUW 6-7 November 2012, ESA 16

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