Methodology for creating software and mathematical support for modeling the spacecraft dynamic operations

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Abstract


The basis for ensuring a high level of reliability and safety in dynamic operations is a comprehensive experimental development of products in conditions as close to the real conditions of operation as possible with the use of mathematical and simulation modeling. The technical task of conducting dynamic operations in orbit is analyzed, which in turn boils down to two basic: bringing the initial state of the spacecraft grouping into a given area of space and performing maneuvers in a given area of space during the active life. These management tasks and terminal requirements are considered to be initial in relation to the stochastic and minimax approaches that are offered for use in the construction of working algorithms. The method of developing a software-modeling complex of the decisive task of developing the means of conducting dynamic operations of the spacecraft has been proposed. The application is illustrated by examples.


About the authors

Veniamin V. Malyshev

Moscow Aviation Institute (National Research University)

Author for correspondence.
Email: veniaminmalyshev@mail.ru
4 Volokolamskoe Shosse, Moscow, 125993, Russian Federation

Head of the Department of System Analysis and Management, Doctor of Technical Sciences, Professor

Alexander V. Starkov

Moscow Aviation Institute (National Research University)

Email: starkov@goldstar.ru
SPIN-code: 5242-3413
4 Volokolamskoe Shosse, Moscow, 125993, Russian Federation

Professor of the Department of System Analysis and Management, Doctor of Technical Sciences

Alexander V. Fedorov

Moscow Aviation Institute (National Research University)

Email: alexanderf@mail.ru
SPIN-code: 6119-3614
4 Volokolamskoe Shosse, Moscow, 125993, Russian Federation

Associate Professor of the Department of System Analysis and Management, Candidate of Technical Sciences

Alexey A. Trishin

Moscow Aviation Institute (National Research University)

Email: trishin0202@mail.ru
4 Volokolamskoe Shosse, Moscow, 125993, Russian Federation

Student of the Department of Information and Control Systems of Aircraft

References

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  4. Malyshev VV, Starkov AV, Tolstenkov PS, Fedorov AV. Methods for maintaining the structure of the high-orbit constellation of spacecraft to compensate for the deterioration of its functionality. Cosmonautics and rocket engineering. 2017;2(95):37—45. (In Russ.)
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Copyright (c) 2021 Malyshev V.V., Starkov A.V., Fedorov A.V., Trishin A.A.

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