This work describes the application of newly developed parallel processing techniques that exploit the irregularly-structured functional parallelism present within a test-bed aerospace system (i.e., a Space Shuttle main rocket engine simulation) utilizing a reduced complexity multicomputing architecture with an arbitrary topology. The methodologies are applicable to real time parallel simulation of large-scale dynamic systems and include deterministic model optimization and decomposition techniques, automated translation mechanisms, and a newly developed task allocation heuristic. The effectiveness of these techniques are illustrated with performance being measured empirically for a wide range of topological configurations using a partially reconfigurable network of Transputers.
Parallel simulation of a large-scale aerospace system in a multicomputer environment
Parallelsimulation eines Large-Scale-Raumfahrtsystems in einer Mehrrechneranlage
IEEE Transactions on Aerospace and Electronic Systems ; 33 , 2, PT.1 ; 507-522
1997
16 Seiten, 12 Quellen
Aufsatz (Zeitschrift)
Englisch
Parallel Simulation of a Large-Scale Aerospace System in a Multicomputer Environment
Online Contents | 1997
|Simulation of multicomputer radar systems for ballistic missile defence
Tema Archiv | 1982
|Prevention of design flaws in multicomputer systems
NTRS | 1977
|