| タイトル | Generation of linear dynamic models from a digital nonlinear simulation |
| 本文（外部サイト） | http://hdl.handle.net/2060/19790008625 |
| 著者（英） | Krosel, S. M.; Daniele, C. J. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1979-02-01 |
| 言語 | eng |
| 内容記述 | The results and methodology used to derive linear models from a nonlinear simulation are presented. It is shown that averaged positive and negative perturbations in the state variables can reduce numerical errors in finite difference, partial derivative approximations and, in the control inputs, can better approximate the system response in both directions about the operating point. Both explicit and implicit formulations are addressed. Linear models are derived for the F 100 engine, and comparisons of transients are made with the nonlinear simulation. The problem of startup transients in the nonlinear simulation in making these comparisons is addressed. Also, reduction of the linear models is investigated using the modal and normal techniques. Reduced-order models of the F 100 are derived and compared with the full-state models. |
| NASA分類 | AERONAUTICS (GENERAL) |
| レポートNO | 79N16796
NASA-TP-1388
E-9490 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/176568 |
