| タイトル | Effects of simplifying assumptions on optimal trajectory estimation for a high-performance aircraft |
| 本文（外部サイト） | http://hdl.handle.net/2060/19900015826 |
| 著者（英） | Belle, Steve D.; Kern, Lura E.; Duke, Eugene L. |
| 著者所属（英） | NASA Dryden Flight Research Facility |
| 発行日 | 1990-04-01 |
| 言語 | eng |
| 内容記述 | When analyzing the performance of an aircraft, certain simplifying assumptions, which decrease the complexity of the problem, can often be made. The degree of accuracy required in the solution may determine the extent to which these simplifying assumptions are incorporated. A complex model may yield more accurate results if it describes the real situation more thoroughly. However, a complex model usually involves more computation time, makes the analysis more difficult, and often requires more information to do the analysis. Therefore, to choose the simplifying assumptions intelligently, it is important to know what effects the assumptions may have on the calculated performance of a vehicle. Several simplifying assumptions are examined, the effects of simplified models to those of the more complex ones are compared, and conclusions are drawn about the impact of these assumptions on flight envelope generation and optimal trajectory calculation. Models which affect an aircraft are analyzed, but the implications of simplifying the model of the aircraft itself are not studied. The examples are atmospheric models, gravitational models, different models for equations of motion, and constraint conditions. |
| NASA分類 | AIRCRAFT STABILITY AND CONTROL |
| レポートNO | 90N25142
NASA-TM-101721
NAS 1.15:101721
H-1597 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/137332 |
|
