| タイトル | A study of space shuttle energy management, approach and landing analysis |
| 本文（外部サイト） | http://hdl.handle.net/2060/19730016103 |
| 著者（英） | Morth, R. |
| 著者所属（英） | Intermetrics, Inc. |
| 発行日 | 1973-04-09 |
| 言語 | eng |
| 内容記述 | The steering system of the space shuttle vehicle is presented for the several hundred miles of flight preceding landing. The guidance scheme is characterized by a spiral turn to dissipate excess potential energy (altitude) prior to a standard straight-in final approach. In addition, the system features pilot oriented control, drag brakes, phugoid damping, and a navigational capacity founded upon an inertial measurement unit and an on-board computer. Analytic formulas are used to calculate, represent, and insure the workability of the system's specifications |
| NASA分類 | SPACE SCIENCES |
| レポートNO | 73N24830
NASA-CR-128937 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/198964 |
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