DocumentCode
3533924
Title
Design space exploration of reconfigurable systems for calculating flying object´s optimal noise reduction paths
Author
Kontos, D. ; Papaefstathiou, I. ; Pnevmatikatos, D.
Author_Institution
ECE Dept., Tech. Univ. of Crete, Chania, Greece
fYear
2009
fDate
Aug. 31 2009-Sept. 2 2009
Firstpage
282
Lastpage
287
Abstract
Despite improved aerodynamic designs that decrease sound emission, the noise produced by flying objects is a problem because it propagates in large distances in the atmosphere. However, it is possible to describe sound propagation effectively with a parabolic differential equation and determine a path that minimizes noise emissions taking into consideration atmospheric and geographic data. This approach calculates noise propagation progressively in the propagation direction and gives accurate results even for large distances. This paper presents a reconfigurable system that solves the tridiagonal problem that results from the Crank-Nicolson function of the 2nd order parabolic equation. Generally tridiagonal algorithms do not allow parallelism in every level, and complicate parallel and/or reconfigurable hardware implementations. We show that reconfigurable hardware technology allows the fast and accurate implementation of such systems. We explore and present several architecture alternatives that pose different tradeoffs. We consider and evaluate different implementations in order to achieve the best possible parallelism and speed with reasonable cost. We find that a large Virtex-5 device is between 9 and 76 times faster than a current desktop PC, depending on the architecture used.
Keywords
acoustic wave propagation; aerospace computing; differential equations; parabolic equations; reconfigurable architectures; 2nd order parabolic equation; Crank-Nicolson function; Virtex-5 device; aerodynamic designs; architecture alternatives; design space exploration; flying object; optimal noise reduction paths; parabolic differential equation; parallel hardware implementation; reconfigurable systems; sound emission; sound propagation; tridiagonal problem; Acoustic noise; Acoustic propagation; Aerodynamics; Atmosphere; Equations; Hardware; Helicopters; Noise level; Noise reduction; Space exploration;
fLanguage
English
Publisher
ieee
Conference_Titel
Field Programmable Logic and Applications, 2009. FPL 2009. International Conference on
Conference_Location
Prague
ISSN
1946-1488
Print_ISBN
978-1-4244-3892-1
Type
conf
DOI
10.1109/FPL.2009.5272288
Filename
5272288
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