Abstract
A new formulation and solution of the problem of calculation of orbits of best approach is discussed. A qualitatively analytical approach to the organization of observations of the motion of artificial Earth satellites is used that makes it possible to calculate and to allow for optimal celestial-mechanics conditions, and to eliminate the effect of systematic observation errors, the effect of the Earth's gravitational field, and other regular perturbations on the solution accuracy.
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Translated from Izmeritel'naya Tekhnika, No. 6, pp. 28–29, June, 1993.
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Makarenko, F.A. The accuracy of calculation of orbits of best approach. Meas Tech 36, 658–661 (1993). https://doi.org/10.1007/BF00980010
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DOI: https://doi.org/10.1007/BF00980010