Method for determining the altitude of an unknown space object to estimate the slant range in problems of orbit calculation from angular optical measurements
Keywords:
space object, optical measurements, orbital parametersAbstract
A method for estimating the altitude of an unknown space object, assuming near-circular orbital motion, is presented. This technique is applied to adjust the slant range parameter and determine two position radius vectors based on optical angular measurements. The initial orbit determination approach utilises two radius vectors from correlated detection regions of the unknown satellite relative to a reference mask satellite. The orbital altitude for the two angular measurement regions of the detected Indefix/Ariane 42p satellite was determined with errors of 2.1 and 2.2 km respectively, compared to the calculated altitude of 752.2 km in the SGP model. By incorporating altitude-based corrections, the slant range error did not exceed 3 km. A comparative analysis was conducted on the initial orbit determination results for the Indefix/Ariane 42p satellite, evaluating the slant range through the projection of linear velocity onto the frame plane and using altitude-based corrections for slant range estimation.
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