KIAM Astrodynamics Toolbox for spacecraft orbital motion design

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Abstract

The KIAM Astrodynamics Toolbox, a new software library for designing spacecraft orbital motion, is introduced. The toolbox is developed at the Keldysh Institute of Applied Mathematics of the Russian Academy of Sciences using Fortran and Python languages, thus combining the computational speed and the flexibility of program design. The library can be useful for space flight mechanics specialists, as well as for students in relevant educational programs.

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About the authors

M. G. Shirobokov

Keldysh Institute of Applied Mathematics of Russian Academy of Sciences

Author for correspondence.
Email: shirobokov@keldysh.ru
ORCID iD: 0000-0002-1747-6430
Russian Federation, Miusskaya sq. 4, Moscow, 125047

S. P. Trifimov

Keldysh Institute of Applied Mathematics of Russian Academy of Sciences

Email: trofimov@keldysh.ru
ORCID iD: 0000-0002-2850-5292
Russian Federation, Miusskaya sq. 4, Moscow, 125047

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Supplementary files

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2. Fig. 1. Graph of variable transformations in the Trajectory class for motion models using ephemerides of celestial bodies.

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3. Fig. 2. Graph of transformations of coordinate systems associated with the Earth, Moon and Sun in the Trajectory class.

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4. Fig. 3. A circular equatorial orbit integrated on one turn in the model of the two-body problem.

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5. Fig. 4. An example of a flat trajectory with low thrust around the Sun.

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6. Fig. 5. Evolution of the eccentricity of the circumlunar orbit in a complex model of motion.

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7. Fig. 6. Low circumlunar orbit with a subsatellite track.

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