| タイトル | Analysis of the Command and Control Segment (CCS) attitude estimation algorithm |
| 本文（外部サイト） | http://hdl.handle.net/2060/19930015533 |
| 著者（英） | Stockwell, Catherine |
| 著者所属（英） | Consolidated Space Test Center|Lockheed Technical Operations Co. |
| 発行日 | 1993-02-01 |
| 言語 | eng |
| 内容記述 | This paper categorizes the qualitative behavior of the Command and Control Segment (CCS) differential correction algorithm as applied to attitude estimation using simultaneous spin axis sun angle and Earth cord length measurements. The categories of interest are the domains of convergence, divergence, and their boundaries. Three series of plots are discussed that show the dependence of the estimation algorithm on the vehicle radius, the sun/Earth angle, and the spacecraft attitude. Common qualitative dynamics to all three series are tabulated and discussed. Out-of-limits conditions for the estimation algorithm are identified and discussed. |
| NASA分類 | COMPUTER PROGRAMMING AND SOFTWARE |
| レポートNO | 93N24722 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/122321 |
