作者: Stefano Pastorelli , Stefano Mauro , Gabriele Biondi , Manuel Mohtar Eizaga Tharek , Mossimo Sorli
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摘要: A system is described for locating the barycenter of at least one object orbiting in space, such as example space debris, adapted to allow physical and mechanical characterization identified object, comprising: remote sensor ( 1 ) placed on board a station 2 detect coordinates certain points (Pi) belonging 3 ), with respect reference system; first means acquiring data related positions assumed time by reconstructing trajectory followed (Pi); second determining instantaneous rotation axes objects associated trajectory, segment perpendicular each pair sequence mean point segment; third computing discrete function d(tk) length segments, an envelope curve (c) local maxima minimum G(tk*) object. process through further described.