Method for calculating the potential of spacecraft elements in 3D space


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Abstract

We propose a method for calculating the potentials of the spacecraft surface, based on triangulation approximation of surfaces, the area method, and analytic calculations of the matrix elements of the Coulomb interaction. The technique described here has a wide range of applications including low, as well as geostationary and polar orbits, and increases the calculating speed and accuracy.

About the authors

N. D. Semkin

Samara State Aerospace University (National Research University)

Author for correspondence.
Email: semkin@ssau.ru
Russian Federation, Moskovskoe sh. 34, Samara, 443086

R. A. Pomel’nikov

Samara State Aerospace University (National Research University)

Email: semkin@ssau.ru
Russian Federation, Moskovskoe sh. 34, Samara, 443086

V. V. Bragin

Samara State Aerospace University (National Research University)

Email: semkin@ssau.ru
Russian Federation, Moskovskoe sh. 34, Samara, 443086

M. A. Rodina

Samara State Aerospace University (National Research University)

Email: semkin@ssau.ru
Russian Federation, Moskovskoe sh. 34, Samara, 443086


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