| タイトル | Space Shuttle ascent guidance, navigation, and control |
| 著者（英） | Thibodeau, J. R., III; Cockrell, B. F.; Long, A. D.; Brand, T. J.; Mchenry, R. L. |
| 著者所属（英） | Draper (Charles Stark) Lab., Inc.|NASA Johnson Space Center |
| 発行日 | 1979-03-01 |
| 言語 | eng |
| 内容記述 | The factors leading to the particular design of the Shuttle guidance, navigation and control software are discussed. The derivation of explicit guidance equations satisfying a wide range of different maneuver constraints and steering equations that create attitude steering errors from the guidance solutions is presented, as are navigation equations, and equations for identifying faulty instruments from sets of redundant instrument measurements. |
| NASA分類 | SPACE COMMUNICATIONS, SPACECRAFT COMMUNICATIONS, COMMAND AND TRACKING |
| レポートNO | 79A32219 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/427554 |
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