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Xilinx Space Heritage Jeff Wetch Aerospace and Defense

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Presentation on theme: "Xilinx Space Heritage Jeff Wetch Aerospace and Defense"— Presentation transcript:

1 Xilinx Space Heritage Jeff Wetch Aerospace and Defense

2 Xilinx Confidential NASA meeting 6/26/06 2 Xilinx in Space Flight Heritage – GRACE (NASA+DLR) – FedSat (Univ. Southern Australia) – OPTUS-C1 (Raytheon) – MARS2003 Lander (JPL) – MARS2003 Rover (JPL) – Venus Express (TU Braunschweig) – HiRise (Ball Aerospace) for MRO ~75 additional programs in various design phases

3 Xilinx Confidential NASA meeting 6/26/06 3 GRACE / NASA + DLR, USA + Germany Sensors PROM Mitigation techniques: None Grace= Gravity Recovery And Climate Experiment Twin Probes to map Earth’s gravity. They will use a microwave beam, depicted by red lines, to track each other. LEO orbit (500kms) XQR4036XL Launched 17mar02 from Plesetsk Cosmodrome / Nth Russia

4 Xilinx Confidential NASA meeting 6/26/06 4 FEDSAT / USA University Re-configurable Computer XQR4062XL Readback Controller PROM Mitigation Techniques: Embedded configuration SEU detection based on Readback Controller Australian Scientific satellite It represents the world’s 1st application of this technology in the harsh environment of outer space “Self Healing Satellite Computer” Near Polar LEO Orbit Altitude: 800 km 58 Kg MicroSat Launched 14dec02 from Tanagashima, Japan

5 Xilinx Confidential NASA meeting 6/26/06 5 OPTUS-C1 / Raytheon, USA DSP applications 18v04 RH Voter Mitigation Techniques: Device Redundancy System Voting and Design Expansion Single source configuration Reconfigure on functional Vote XQVR300 UHF payload designed and manufactured by Raytheon St Peterburg, Florida. Largest hybrid Commercial & Defense Communications satellite. GEO orbit at 156 E Longitude Virtex FPGAs are used to apply Signal Process algorithms to communications data coming from Earth. Launched 6nov03

6 Xilinx Confidential NASA meeting 6/26/06 6 Mars 2003 Lander & Rover – Xilinx used for Mission-critical systems – Lander: Pyrotechnics, retro- rockets, parachute deployment, & explosive bolts. – Rover: All motor controllers – Operated through worst Solar Flare ever measured Launched in Jul03

7 Xilinx Confidential NASA meeting 6/26/06 7 Example: MER Pyro Control Launched in Jul03

8 Xilinx Confidential NASA meeting 6/26/06 8 MER 2003 Lander / JPL, USA Pyrotechnic board XQR4062XL Readback Controller XQR4062XL Readback Controller XQR4062XL Readback Controller XQR4062XL Readback Controller Pyro Relay 1701L Launched in Jul03

9 Xilinx Confidential NASA meeting 6/26/06 9 MER 2003 ROVER / JPL, USA Motor Controller XQVR CG560V PROM PRC Mitigation Techniques: System cycled once per Martian Evening Readback for SEU detection Scrubbing for SEU correction Operating successfully since the 04jan2004 Launched in Jul03

10 Xilinx Confidential NASA meeting 6/26/06 10 MRO 2005 HiRise Camera XQVR300E -4CB228M PROM Mitigation Techniques: System cycled periodically Readback for SEU detection Scrubbing for SEU correction Launched in Jul03 PRC

11 Xilinx Confidential NASA meeting 6/26/06 11 Venus Express TU Braunschweig, Germany Image Processing (VMC Venus express Monitoring Camera) Mitigation Techniques: XQVR600-4CB228M EDAC + TMR + Scrubbing Customer paper: « To maintain correct operation in the presence of SEU errors, extensive EDAC functions are implemented. All application specific functional blocks are implemented using TMR design. The most important measure is to scrub the configuration in short time intervals to eliminate the SEU effects. A complete processor reconfiguration is scheduled every hour to avoid accumulation of persistent errors… ». Launched 09nov05 from Baikonour

12 Xilinx Confidential NASA meeting 6/26/06 12 CIBOLA / Los Alamos & SSTL, USA & England Remote Sensing PROM Comp.PRC Mitigation Techniques: Dual Redundancy for error detection Partial Configuration error detection and correction Instrument used to monitor ionospheric and lightning effects on UHF VHF radio spectra LEO Orbit Part of DoD STP-1 spacecraft scheduled to launch in mid 2006 Launch expected by Mid-06

13 Xilinx Confidential NASA meeting 6/26/06 13 ISS-Columbus payload FSL / Verhaert, Belgium PROM Mitigation techniques: None FSL= Fluid Science lab LEO orbit (400kms) XQR4013XL Launched expected Mid-07

14 Xilinx Confidential NASA meeting 6/26/06 14 ISS-Columbus payload EuTEMP / EFACEC, Portugal PROM  EuTEMP mission: Mission: to develop a system capable of monitor and record the temperature of the pallet experiences EuTEF during the transfer from the Space Shuttle to the ISS (Columbus external pallet).  LEO orbit (400kms) XQ4036XL Launched expected Mid-07

15 Xilinx Confidential NASA meeting 6/26/06 15 ISS / EADS Astrium, Germany Camera System PROM Mitigation techniques: None LEO orbit (400kms) XQR4036XL Launched expected Mid-07

16 Xilinx Confidential NASA meeting 6/26/06 16 ATV / EADS-ST, France PROM Mitigation techniques: None ATV= Automated Transfer Vehicle LEO orbit (400kms) 1st Flight expected 2006 XQR4013XL Launch OF 1st ATV « Jules Verne » expected by mid-07

17 Xilinx Confidential NASA meeting 6/26/06 17 ComSAT2 & SarLUPE / OHB System, Germany Image Processing PROM Mitigation Techniques: Readback XQVR300/600

18 Xilinx Confidential NASA meeting 6/26/06 18 General Dynamics, USA Classified Project/Application PROM PRC Mitigation Techniques: TMR used for state- machine logic only.

19 Xilinx Confidential NASA meeting 6/26/06 19 CMIS / Boeing, USA Image Processing Virtex-II PROM Mitigation Techniques: System cycled once per minute Boeing has contract for 2-4 CMIS instruments CMIS (Conical Microwave Imager Sounder) Part of NPOESS Program owned by DoD and NOAA First instrument delivered in 2005, second in 2007 LEO Orbit Launch expected by 2008

20 Xilinx Confidential NASA meeting 6/26/06 20 Xilinx in Space Next to launch – CrIs (ITT) XQR2V6000 – Birch (ITT) XQR2V6000 – Hifes (Sandia) XQR2V3000 – Cayman (Boeing) XQVR300 – DRP (General Dynamics) XQR2V3000 Etc….. + Other Classified Projects


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