SDI (Satellite Data Ingestor) 2015 McIDAS Users Group Meeting June 8, 2015.

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Presentation transcript:

SDI (Satellite Data Ingestor) 2015 McIDAS Users Group Meeting June 8, 2015

Overview  SDI 104  Hardware configuration  Software configuration  Satellites signals  Next generation SDI  Hardware Configuration  Software configuration  Satellites signals

SDI 104 Hardware Configuration  PC/104-Plus  LittleBoard 735  1 GHz CPU  Disk: 160 Gbyte IDE  Boot from compact flash  Ethernet: Up to 1G/s  Connectors for monitor and keyboard  Mounted in 2U rack box

Hardware Configuration Data rates tested up to 40 Mbits/s  Connectors: –D15P –BNC  Configuration: –Single ended (TTL) –RS422 (differential)  Data types –NRZ-L, NRZ-M, NRZ-S –Jumper configurable

Software Configuration  Knoppix (Linux )  Up-to-date security  Compatible with old binaries  Upgrade to Knoppix for older SDI-104 systems running DSL as needed  Can be configured as a standalone ingestor/server, or write data to an external disk (via NFS, for example)

Event Notification  Notifications are dependent on signal type: – Image start (not for POES) – Image end (not for GVAR Imager)  Three types of notifications: – Send an – Write notification to a file (log messages) – Run a program or script

SDI-104 Status for Current Satellites  GVAR: up-to-date for entire series  MTSAT: up-to-date for both satellites ‑ May want to add swap space if running DSL (noisy data)  POES AVHRR:  Up-to-date for all satellites  Unable to test direct reception, although a system is running at NWS Honolulu

(Original) SDI Sunset The Original SSEC SDI was sunset on 31 December 2013  We are not able to provide nor recommend hardware components if these would fail  The operating system used is an unsupported version of Solaris, which has been lacking security updates for several years.

SDI … the next generation

Introducing the SDI-SE

SDI-SE Hardware Configuration*  Dell PowerEdge R430 servers  12 core, 2.5 GHz Intel Xeon Processor  64 GB Ram  6 1-TB disks in RAID-6  10 Gb Ethernet and 1 GB Ethernet  No more clock and data  Everything over ethernet (no SSEC designed hardware components) *preliminary

SDI-SE Software Configuration*  CentOS 6.x  Software and security updates via yum  Repository at UW SSEC  McIDAS-X ADDE servers  CSPP-GEO ingest software  RabbitMQ event notification *preliminary

SDI-SE Data Access*  ADDE  FTP *preliminary

SDI-SE Event Notification*  RabbitMQ  Built in exchange server  Start and End Events  No more events  Remote workstations will be able to connect to the Exchange server and receive desired events  May update SDI-104 to use RabbitMQ in the future *preliminary

SDI-SE Supported Satellites *  GOES-R series  Ingest handled by CSPP GEO  Instruments  ABI (Advanced Baseline Imager)  Follow/tracking  GLM (Geostationary Lightning Mapper)  MAG (Magnetometer)  SEISS (Space Environment In-Situ Suite)  SUVI (Solar Ultraviolet Imager)  EXIS (Extreme Ultraviolet and X-ray Irradiance Sensors)  No Level-2 processing on the SDI-SE  HimawariCast (under consideration)  GVAR (under consideration) *preliminary

What is CSPP – GEO?  Community Satellite Processing Package for Geostationary Data  NOAA sponsored project being developed at UW SSEC  The software will be capable of processing GOES Rebroadcast (GRB) data received from the next-generation GOES-R satellite. Level 2 Advanced Baseline Imager (ABI) products will be generated by state-of-the-art science algorithms developed under the GOES-R Algorithm Working Group project.  Software is freely available and is distributed as self- contained binary packages built for 64-bit Linux systems.

CSPP – GEO initial product suite  Cloud mask  Cloud phase  Cloud type  Cloud top height  Cloud top temperature  Cloud top pressure  Cloud 11 µm emissivity  Cloud visible optical depth  Cloud effective radius  Cloud liquid water path  Cloud ice water path  Probability of Marginal Visual Flight Rules (MVFR)  Probability of Instrument Flight Rules (IFR)  Probability of Low Instrument Flight Rules (LIFR)  Low cloud geometric thickness

End