Method for calculating earliest time of Beidou medium earth orbit satellite graveyard orbit to cross orbits of other global satellite navigation systems
A global satellite navigation and satellite technology, applied in satellite radio beacon positioning systems, radio wave measurement systems, measurement devices, etc., can solve problems that do not involve time travel
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[0047] In order to make the technical problems, technical solutions and beneficial effects solved by the present invention clearer, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention.
[0048] to combine figure 1 , the present invention provides a method for calculating the time when the Beidou mid-orbit satellite graveyard orbit crosses the orbit of other global satellite navigation systems the earliest, comprising the following steps:
[0049] Step 1: Calculate the eccentricity threshold;
[0050]When the perigee or apogee of the graveyard orbit of the Beidou medium-orbit satellite passes through other global navigation constellation orbits, the corresponding eccentricity is the threshold value, and the perigee and apogee expressions are as follows: ...
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