Article ID: | iaor1995161 |
Country: | United States |
Volume: | 61 |
Issue: | 1 |
Start Page Number: | 53 |
End Page Number: | 59 |
Publication Date: | Jul 1993 |
Journal: | ACM SIGPLAN Notices |
Authors: | Fritchman B.M., Hammond R.A. |
Keywords: | simulation: applications |
The emergence of electronic flight-control systems into commercial aircraft designs has precipitated an immediate need for nonlinear, discrete-time analyses in both frequency and time-domains, for both the aircraft Structural Dynamic Loads and the Flight Controls communities. This paper presents and demonstrates a methodology by which the large-scale, linear aircraft structural models produced by the Structural Dynamic Loads community can be easily reformulated using EASY5