FIELD: aircraft engineering.
SUBSTANCE: proposed method comprises generation of virtual fragment of space debris in compliance with mass preservation law with application of the model of failure to debris to object resulted from said failure. Orbit of every virtual space debris fragment is computed during observation at stationary point with application of the model of debris path to said virtual fragment. Proceeding from the results of orbit computation, distribution of frequency of debris every virtual fragment vector of motion in coelosphere is generated. Proceeding from said vector search range vector is set with upper level of distribution of motion vector frequency. Used the method of overlay to areas in images fixed at time intervals during observation in stationary point.
EFFECT: detection of space debris in geocentric orbit.
5 cl, 12 dwg
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Authors
Dates
2014-12-20—Published
2011-09-08—Filed