| タイトル | An on-board near-optimal climb-dash energy management |
| 本文（外部サイト） | http://hdl.handle.net/2060/19830008058 |
| 著者（英） | Kelley, H. J.; Cliff, E. M.; Weston, A. R. |
| 著者所属（英） | Virginia Polytechnic Inst. and State Univ. |
| 発行日 | 1982-12-01 |
| 言語 | eng |
| 内容記述 | On-board real time flight control is studied in order to develop algorithms which are simple enough to be used in practice, for a variety of missions involving three dimensional flight. The intercept mission in symmetric flight is emphasized. Extensive computation is required on the ground prior to the mission but the ensuing on-board exploitation is extremely simple. The scheme takes advantage of the boundary layer structure common in singular perturbations, arising with the multiple time scales appropriate to aircraft dynamics. Energy modelling of aircraft is used as the starting point for the analysis. In the symmetric case, a nominal path is generated which fairs into the dash or cruise state. Feedback coefficients are found as functions of the remaining energy to go (dash energy less current energy) along the nominal path. |
| NASA分類 | AIRCRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 83N16329
NAS 1.26:169755
NASA-CR-169755 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/163774 |
