
The paper considers the phase methods for measuring an object spatial orientation by means of satellite navigation equipment. Methods for the resolution of phase ambiguity are analyzed. Effectiveness and applicability of the one-step methods are discussed in more detail. It is proved that for the realization of the exhaustion method the minimal group of navigation space crafts should include 5–6 observed ones. When measuring signals of 8 space crafts with base length of 1 m, an unambiguous solution is achieved practically in all cases.
Текст статьи не публикуется в открытом доступе в соответствии с политикой журнала.
interferometer, satellite navigation systems, single-step exhaustion methods, the phase ambiguity, 47.49.31
interferometer, satellite navigation systems, single-step exhaustion methods, the phase ambiguity, 47.49.31
| selected citations These citations are derived from selected sources. This is an alternative to the "Influence" indicator, which also reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically). | 0 | |
| popularity This indicator reflects the "current" impact/attention (the "hype") of an article in the research community at large, based on the underlying citation network. | Average | |
| influence This indicator reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically). | Average | |
| impulse This indicator reflects the initial momentum of an article directly after its publication, based on the underlying citation network. | Average |
