| タイトル | Two locations, two times, and the element set |
| 著者（英） | Taff, L. G.; Randall, P. M. S. |
| 著者所属（英） | Massachusetts Inst. of Tech. |
| 発行日 | 1985-10-01 |
| 言語 | eng |
| 内容記述 | A robust analytical formulation is developed to apply classical initial orbital determination to artificial satellites whose locations are uncertain to about 1 cu km and separated in time by no more than 30 min. An analytical simplification reduces Gauss's method, iteration on the semilatus rectum, iteration on the true anomaly, and the Lambert-Euler technique, to the solution of a single equation in one unknown, instead of the usual coupled triplet of three equations in three unknowns. The method is demonstrated for all common artificial satellite orbits over a variety of time intervals between the two location vectors, and for a varied set of position and distance errors. |
| NASA分類 | ASTRODYNAMICS |
| レポートNO | 86A39586
AD-A170553
ESD-TR-86-076 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/384270 |
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