| タイトル | GEODYN programmer's guide, volume 2, part 2 |
| 本文（外部サイト） | http://hdl.handle.net/2060/19750003344 |
| 著者（英） | Goad, C. C.; Mullins, N. E.; Chin, M. M.; Martin, T. V.; Boulware, N. L.; Dao, N. C. |
| 著者所属（英） | Wolf Research and Development Corp. |
| 発行日 | 1972-10-01 |
| 言語 | eng |
| 内容記述 | A computer program for executive control routine for orbit integration of artificial satellites is presented. At the beginning of each arc, the program initiates required constants as well as the variational partials at epoch. If epoch needs to be reset to a previous time, the program negates the stepsize, and calls for integration backward to the desired time. After backward integration is completed, the program resets the stepsize to the proper positive quantity. |
| NASA分類 | EARTH RESOURCES AND REMOTE SENSING |
| レポートNO | 75N11416
NASA-CR-139151 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/192177 |
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