Title :
Using many-core processors to improve the performance of space computing platforms
Author :
Kraja, Fisnik ; Acher, Georg
Author_Institution :
Comput. Archit., Tech. Univ. Munchen, Munich, Germany
Abstract :
Taking into consideration space applications´ demands for higher bandwidth and processing power, we propose to efficiently apply upcoming many-core processors and other Commercial-Off-The-Shelf (COTS) products to improve the on-board processing power.1 2 A combination of traditional hardware and software-implemented fault-tolerant techniques, addresses the reliability of the system. We first describe common requirements and design challenges presented by future space applications like the High Resolution Wide Swath Synthetic Aperture Radar (HRWS SAR). After proposing the High Performance Computing (HPC) architecture, we compare between most suitable hardware technologies and give some rough performance estimations based on their features. For benchmarking purposes we have manually converted the Scalable Synthetic Compact Application (SSCA#3) from Matlab to C and parallelized it using OpenMP. It turns out that this application scales very well on many-core processors especially on a distributed Shared Memory Architecture (SMA).
Keywords :
aerospace computing; distributed shared memory systems; mathematics computing; multiprocessing systems; performance evaluation; synthetic aperture radar; Matlab; OpenMP; commercial-off-the-shelf product; distributed shared memory architecture; hardware implemented fault tolerant technique; high performance computing architecture; high resolution wide swath synthetic aperture radar; many-core processor; on-board processing power; performance estimation; scalable synthetic compact application; software implemented fault tolerant technique; space computing; Bandwidth; Computer architecture; Fault tolerance; Fault tolerant systems; Hardware; Program processors; Tiles;
Conference_Titel :
Aerospace Conference, 2011 IEEE
Conference_Location :
Big Sky, MT
Print_ISBN :
978-1-4244-7350-2
DOI :
10.1109/AERO.2011.5747445