On-Board Data Handling for the PAMELA Experiment - PowerPoint PPT Presentation

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On-Board Data Handling for the PAMELA Experiment

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9 radiator planes (Cfibres) straws tubes (Xe/CO2). Separazione 102 e/p (E ... DLink S/C. R.Wischnewski. The PSCU is constructed in 2 phases by LABEN/Milano: ... – PowerPoint PPT presentation

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Title: On-Board Data Handling for the PAMELA Experiment


1
On-Board Data Handling for the PAMELA Experiment

Ralf Wischnewski Roma2 DESY-Zeuthen
Alghero, 30.9.2002
2
  • The task
  • Space requirements
  • Pamela CPU PSCU
  • On-board DAQ design
  • Data downlink
  • Status Summary

3
The INSTRUMENT
4
The Tasks (1)
5
The Tasks (2)
6
PAMELA STORAGE AND CONTROL UNIT
  • CPU (ERC32 SPARC V7) 17 Mips _at_ 24MHz
  • SRAM 4 Mbyte
  • Boot PROM
  • EEPROM 1 Mbyte
  • 1553 Remote Terminal to Satellite CPU
  • 64 Kb x 16 RAM buffer
  • Logic ASIC which include PCMCIA
  • bus controller Parallel System Bus
  • Solid State Mass Memory 2 2 Gbytes
  • Pamela Interface (PIF) DMA bus controller and
    TAM interface
  • Telemetry Housekeeping board 32 outputs 78
    inputs
  • DC/DC converter integrato da 27 V a 14.4 V 5.2
    V
  • Quartz clock 1 ms

7
PAMELA DAQ Schematics
8
PAMELA DAQ Schematics
Detectors
9
Data Downlink to S/C and Earth
  • Science and HK data (1-2 GB) to be transfered
    from Pamela to Satellite MassMemory (gt100GB)
    every few hours.
  • Asynchronous request from Master S/C-CPU.
  • Downlink from S/C to earth during ground station
    passages (Moscow Sturup/Sweden) _at_ 320Mbps over
    a few minutes.
  • Needs fast analysis for uplink response on next
    orbit.
  • All operations based on pre-defined absolute
    time schedule, arbited from S/C and uplinked from
    Ground.


10
Pamela Data PathS/C to Ground
MM S/C
DLink S/C
11
PSCU Engineering Model
RAM (2x2 GB)
CPU, PIF, TMTC
DCDC
The PSCU is constructed in 2 phases by
LABEN/Milano 1. Engineering Model (EM),
currently under full test _at_ INFN 2.
Flight Model (FM), under construction _at_ LABEN
12
PAMELA ENGINEERING MODEL
  • Assembly of the Engineering Model (EM) is the
    major functionality and I/F test to be passed
    before the final Flight Model (FM) is build
  • System compability test
  • Mechan. electr. interface test
  • Test procedure definiton for ground test
    equipment (EGSE).

Note The PSCU is (with Power Supply) the main
Interface between Pamela and the Satllite.
13
PSCU-EM Tests
  • Basic functionality test
  • Trigger rate 80 Hz
  • 1/10 evts transfered to CPU-RAM
  • to simulate sampled event analysis
  • Telecomand communication
  • (1553 Bus)
  • Write to PSCU MassMemory
  • and download via TAM


14
PSCU TEST EQUIPMENT
  • Full functionality test of PSCU needs an
  • Electrical Ground Support Equipment (EGSE),
  • simulating all system interfaces
  • power supply (27 V)
  • Control Command (ON/OFF, RESET)
  • bus 1553 for telecomands
  • telemetry
  • I-DAQ board to receive FE Comands and
  • reply detector data in real time
  • monitor for PSCU electrical/thermal status
  • debugger and monitoring SW
  • simulator for Housekeeping input
  • event trigger simulation
  • science data readout (TAM)

15
PSCU TEST EQUIPMENT _at_ ROMA
16
PSCU - ON-BOARD SOFTWARE
  • RTEMS as Operation System
  • (Real-Time Executive for Multiprocessor
    systems)
  • multitasking
  • preemptive or monotonic scheduling
  • comunication zone and intertask synchronisation
  • interrupt handling
  • optional task interrupt priority
  • dynamic memory allocation
  • RTEMS is supported by ESA/ESTEC including Cross
    Compiler ERC32CC with
  • GNU C compiler
  • Linker, assembler, archiver etc.
  • Standalone C-library
  • RTEMS real-time kernel with ERC32 BSP
  • ERC32 boot-prom utility
  • Standalone simulator ERC32
  • GNU debugger with ERC32 simulator DDD

17
Main Functional Modes and Tasks
Overview of Pamela main functional modes and
parallel system tasks. Telecomands from S/C
Master CPU switch between operation modes.
Automatic-mode change is under implementation. TMT
C-Housekeeping, S/C 1553 I/F, Logging, Error
check and General Interrupt handling tasks are
permanentely active.
18
Science data event managment chart
19
BEAM TEST _at_ CERN SPS 5-12/06/2002
e _at_ 20-300 GeV p _at_ 300-350 GeV
PSCU Buffers are optimized for event size lt 16
kB.
Tracker data size (compressed).
20
Second Level Trigger
Trigger on IDAQ-Board Fast DSP-rejection
algorithm for Background events, w/o PSCU.
Using AntiCoincidence Veto. But signal
rejection by back- scattering from
calorimeter. Calorimeter - particle
classification (non-interacting, hadronic,
em). TOF - n of hits per plane TRACKER - n of
clusters, no online reconstruction. Verificati
on with SPS/PS test beam data (2002).
21
PAMELA DAQ - Summary
  • Most components of the Pamela DAQ and Slow
    Control are ready for system test.
  • CPU-EM in full test _at_ INFN CPU-FM in production
    _at_Laben
  • Finalization of Pamela Slow Autonomous Control
    Procedures
  • Next steps
  • DAQ / FE-board system test with S/C-Simulator
    in Rome (12/2002)
  • Deliver Pamela-EM to Russia for S/C EM test
    (1/2003)
  • Integration of Pamela FM with FM-PSCU, physics
    test, delivery to Russia (5/2003).
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