GEO target multipoint preferred short arc orbit determination method based on space-based optical observation data
An observation data and optical technology, applied in the aerospace field, can solve the problems such as the inability to guarantee the convergence and accuracy of the initial orbit of the short arc, and the short arc of the GEO target observation.
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[0096] Table 1 Accuracy and success rate of GEO short-arc orbit determination for space-based optical surveillance
[0097]
[0098] The results in Table 1 are based on the common sun-synchronous orbit space-based optical surveillance platform as the simulation scene to patrol and observe 3235 arcs of GEO targets, each observation lasts about 3 minutes, and the observation accuracy of right ascension and declination is about 10 arc seconds . Among them, the success rate of orbit determination is the proportion of the number of successful arcs of the specified orbit. Among them, the failure of orbit determination mainly includes the failure to converge to obtain the number of orbits, the orbit converges to a trivial solution, and the error of the semi-major axis of the orbit is too large (the semi-major axis error is defined in this paper. Long axis error ≥ 1000km), etc. It can be seen from Table 1 that the semi-major axis orbit determination accuracy of the method in this ...
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