| タイトル | Continuation Methods for Qualitative Analysis of Aircraft Dynamics |
| 本文（外部サイト） | http://hdl.handle.net/2060/20040110969 |
| 著者（英） | Cummings, Peter A. |
| 著者所属（英） | National Inst. of Aerospace; NASA Langley Research Center |
| 発行日 | 2004-07-01 |
| 言語 | eng |
| 内容記述 | A class of numerical methods for constructing bifurcation curves for systems of coupled, non-linear ordinary differential equations is presented. Foundations are discussed, and several variations are outlined along with their respective capabilities. Appropriate background material from dynamical systems theory is presented. |
| NASA分類 | Aircraft Stability and Control |
| レポートNO | NIA-2004-06
NASA/CR-2004-213035 |
| 権利 | No Copyright |
