| タイトル | Optimal RTLS abort trajectories for an HL-20 personnel launch vehicle |
| 本文（外部サイト） | http://hdl.handle.net/2060/19940020632 |
| 著者（英） | Dutton, Kevin |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1993-12-01 |
| 言語 | eng |
| 内容記述 | The primary objective of this study was to determine whether Return To Launch Site (RTLS) abort at T seconds along the launch trajectory of the Personnel Launch System (PLS) is possible using optimal control theory. The secondary objective is to assess effects of bank angle constraint, lift coefficient constraint, free and fixed final boundary conditions, etc. of the vehicle. The PLS is a complementary system to the Space Shuttle. |
| NASA分類 | ASTRODYNAMICS |
| レポートNO | 94N25114 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/113515 |
|
