FIELD: cosmonautics. SUBSTANCE: apparent position and apparent size of first approaching space vehicle at each successive moment t1 and t2 are determined and position of reference point of second approaching space vehicle is calculated; then components of relative velocity of second approaching space vehicle relative to first approaching space vehicle and coordinates of position of reference point connected with second approaching space vehicle at any moment of time "t" are calculated. EFFECT: enhanced accuracy of determination. 10 cl, 3 dwg
Authors
Dates
1998-01-27—Published
1993-03-15—Filed