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Contents FLIPPER Product SheetSuitability of reprogrammable FPGAs in space applicationsFunctional Triple Modular Redundancy (FTMR)Lessons learned from FPGA developmentsESA FPGA task force: Lessons learned About us
Technologies for Space ESA IP Cores
ASIC Developments History System Level Modeling
| ||The use of reprogrammable FPGAs in space|
Reprogrammable (SRAM based) FPGA (RFPGA), featuring high flexibility, combined with high performance and complexity become increasingly important also for space applications. With satellite lifetimes increased far beyond 10 years, much longer than the validity of telecom standards, reprogrammability in flight becomes a stringent requirement. If software solutions are not possible, RFPGA may soon be the only solution.
Notwithstanding to the general methodology and recommendations outlined in the documents in the "Microelectronics Development Methodology" page, which are mostly applicable to FPGAs as well, specific considerations apply to the use of FPGA in space.
This is mostly due to the fact that, in contrary to ASIC or one-time (antifuse) programmable FPGA, the configuration of RFPGA is stored in an SRAM, which is sensitive to SEU's. The radiation behaviour of RFPGA and methods for SEU mitigation is investigated in several studies.
This page also presents lessons learned from space FPGA developments not directly related to radiation-induced issues.
FLIPPER Product Sheet
The FLIPPER test system has been developed by IASF Milano under an ESA contract. FLIPPER allows the injection of SEU-like faults into the user flip-flops, configuration memory and reconfiguration control registers of a Xilinx FPGA. This allows for the impact of configuration SEUs on unprotected designs to be tested, as well as the efficiency of fault mitigation methods to be evaluated.
The Executive Summary of this activity is available for download, along with a Product Sheet.
Author: Monica Alderighi, IASF – INAF, Milano (pdf available)
Suitability of reprogrammable FPGAs in space applications
"Field Programmable Gate Array (FPGA) devices have been used in space for more than a decade with a mixed level of success. Until now, few reprogrammable devices have been used on European spacecraft due to their sensitivity to involuntary reconfiguration due to Single Event Upsets (SEU) induced by radiation. But with the advent of reprogrammable devices featuring a million systemgates or more, it is not longer feasible to disregard these technologies."
This document concentrates on SRAM based FPGA devices from Xilinx. Through a comprehensive bibliography, it illustrates SEU failure mechanisms and susceptibility, SEU mitigation approaches and summarises (radiation) test results. Author: Sandi Habinc (pdf available)
Functional Triple Modular Redundancy (FTMR)
"VHDL Design Methodology for Redundancy in Combinatorial and Sequential Logic"
Further expands the 'logic replication and voting in combinatorial and sequential logic', mentioned in the previous document. In particular implementing redundancy in combinatorial logic is a challenge, since commercial synthesis tools aim to remove any logic redundancy. A VHDL coding method is developed, which reliably allows to infer configurable levels of redundancy in registers and combinatorial logic. Code examples are given as well as synthesis and layout results. Author: Sandi Habinc (pdf available)
Lessons learned from FPGA developments
"The complexity of the designs that are made in FPGAs has increased at the same rate as for ASICs. In essence, the FPGA design task has become much more complex. It has never before been so easy to make so many mistakes so fast as now."
Starting from a summary of things which went wrong in real life ("lessons learned"), this document is an extension to the two previous documents, suggesting a development/design methodology for FPGA and valuable recipees for single event mitigation in FPGA designs.Author: Sandi Habinc (pdf available)
ESA FPGA task force: Lessons learned
This paper gives an overview of the audits that ESA made on several FPGA designs included in the Rosetta spacecraft. and to assess any potential problems and their solutions at spacecraft and/or operational level. MAPLD, September 2002. Authors A. Fernandez-Leon, A. Pouponnot, S. Habinc (pdf available)
Last update: 4 March 2013
Related documentsFLIPPER Executive Summary (pdf)FLIPPER Product Sheet (pdf)Suitability of reprogrammable FPGAs in space applications (pdf)Functional Triple Modular Redundancy, FTMR (pdf)Lessons learned from FPGA Developments (pdf)ESA FPGA task force: Lessons learned (pdf)