| タイトル | Aircraft flight test trajectory control |
| 本文（外部サイト） | http://hdl.handle.net/2060/19890018045 |
| 著者（英） | Walker, R. A.; Menon, P. K. A. |
| 著者所属（英） | Integrated Systems, Inc. |
| 発行日 | 1988-09-01 |
| 言語 | eng |
| 内容記述 | Two control law design techniques are compared and the performance of the resulting controllers evaluated. The design requirement is for a flight test trajectory controller (FTTC) capable of closed-loop, outer-loop control of an F-15 aircraft performing high-quality research flight test maneuvers. The maneuver modeling, linearization, and design methodologies utilized in this research, are detailed. The results of applying these FTTCs to a nonlinear F-15 simulation are presented. |
| NASA分類 | CYBERNETICS |
| レポートNO | 89N27416
NASA-CR-4161
NAS 1.26:4161
H-1497 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/140951 |
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