STUDY OF TECHNOLOGY FOR THE RELIABILITY AND SURVIVABILITY MODELLING OF ONBOARD CONTROL SYSTEM OF SMALL SPACECRAFT OPERATING IN COMPLEX MODES

Alexander N. Pavlov; Dmitry A. Pavlov; Alexander Yu. Kulakov; Valerii V. Zakharov

doi:10.5937/jaes0-50149

Alexander N. Pavlov Mozhaisky Military Aerospace Academy, St. Petersburg, Russia; Saint Petersburg Federal Research Center of the Russian Academy of Sciences, St. Petersburg, Russia https://orcid.org/0000-0002-6193-8882
Dmitry A. Pavlov Mozhaisky Military Aerospace Academy, St. Petersburg, Russia https://orcid.org/0000-0002-9238-9505
Alexander Yu. Kulakov Saint Petersburg Federal Research Center of the Russian Academy of Sciences, St. Petersburg, Russia https://orcid.org/0000-0002-4665-7273
Valerii V. Zakharov Saint Petersburg Federal Research Center of the Russian Academy of Sciences, St. Petersburg, Russia https://orcid.org/0000-0002-2086-2041

DOI: https://doi.org/10.5937/jaes0-50149

Keywords: modes of functioning, parametric genome of structure, structural and functional survivability, motion control system, small spacecraft, onboard control complex

Abstract

The technology of system modeling of reliability and survivability of the onboard control system (OCS) of the spacecraft is presented in the study of various options for the activation of operating modes. The technology of spacecraft functioning based on the concept of digital twins currently takes a leading position. That’s concept allows you to create realistic virtual copies of spacecraft, to simulate not only the objects themselves, but also the processes of their design and operation in various conditions of a priori uncertainty. Such conditions, first of all, should include the destructive effects of an aggressive external environment (outer space) and the multi-mode nature (sequence and intensity of the modes involved) of the functioning of onboard spacecraft systems. The implementation of the requirements of multi-purpose and multi-mode control in these conditions is closely related to the study of the reliability and survivability of such objects from the standpoint of considering their structural construction. The proposed article discusses an approach to assessing the reliability and survivability of onboard systems of small spacecraft (SS), which is based on the concept of a parametric genome structure, taking into account the multi-mode operation in an aggregated form.

References

Kolodezhny, L. P., Chernodarov, A. V. (2010). Reliability and technical diagnostics. Publishing house of VVA named after N. E. Zhukovsky and Yu. A. Gagarin, pp. 452.

Kalinov, M. I., Rodionov, V. A. (2019). Substantiation of the choice of a rational option for the use of small spacecraft in case of failure of individual elements of their onboard systems. IX All-Russian scientific and practical conference on simulation modeling and its application in science and industry (IMMOD-2019), pp. 434-438.

Raikunov, G. G. (2010). Ionizing radiation from outer space and their impact on the onboard equipment of spacecraft. M. Fizmatlit, pp. 256.

Yarmolik, V. N., Vashinko, Yu. G. (2011). Physically non-clonable functions. Informatics, No2, pp.92-103.

Pavlov, A. N., Pavlov, D. A., Aleshin, E. N., Vorotyagin, V. N., Umarov, A. B. (2021). Modeling and analysis of structural and functional reliability of complex multi-mode objects. SPb.: Proceedings of the VKA named after A. F. Mozhaisky, No 677, pp. 186-194.

Pavlov, A.N., Pavlov, D.A., Vorotyagin, V.N., Umarov, A.B. (2020). Structural and Functional Analysis of Supply Chain Reliability in the Presence of Demand Fluctuations // Models and Methods for Researching Information Systems in Transport 2020 , pp. 61-66, MMRIST.

Pavlov, A. N., Umarov, A. B., Aleshin, E. N. (2021). Study of the structural significance of supply chain elements with variable order rate. SPb: Intelligent Transport Systems. Transport Security – 2021, pp.25-32.

Pavlov, A. N., Vorotyagin, V. N., Slinko, A. A. (2019). Methodology for assessing the structural and functional survivability of onboard systems of small spacecraft in the conditions of the occurrence of off-design flight situations. Information and Space, No 2, pp. 139-147.

Pavlov, A. N., Vorotyagin, V. N., Kulakov, A. Yu., Umarov, A. B. (2020). Investigation of the structural and functional reliability of small spacecraft when solving orientation problems. Informatization and communication, No 4, pp. 156-164.

Pavlov, A.N., Aleshin, E.N., Zinov'ev, S.V., Kopkin, E.V., Osipenko, S.A., Sokolov, B.V. (2018). System analysis of organizational and technical systems for space application. SPb.: VKA named after A. F. Mozhaisky, pp. 357-360.

Filatov, A. V., Tkachenko, I. S., Tyugashev, E. V., Sopchenko, E. V. (2015). Mathematical support of the motion control system of small spacecraft. Information technologies and nanotechnologies. Samara State Aerospace University named after academician S. P. Korolev (National Research University), pp. 290-294.

Goh, M., Lim, J. Y. S., Meng, F. (2007). A stochastic model for risk management in global chain networks. European Journal of Operational Research 182 (1), 164–173.

Akimov, E. V., Kuznetsov, M. N. (2010). Probabilistic mathematical models for assessing the reliability of wireless sensor networks. Proceedings of MAI, No 40, p. 16.

Polenin, V.I., Ryabinin, I.A., Svirin, S.K., Gladkov, I.A.; Mozhaev, A.S. (2011). Application of the general logical-probabilistic method for the analysis of technical, military organizational-functional systems and armed confrontation: monograph, scientific publication. SPb.: SPb-regional department of the Russian Academy of Natural Sciences, pp. 416.

Kopytov, E.A., Pavlov, A.N., Zelentsov, V.A. (2010). New methods of calculating the Genome of structure and the failure criticality of the complex objects’ elements // Transport and Telecommunication, vol. 11, No 4, pp. 4-13.

Pavlov, A., Ivanov, D., Dolgui, A., Sokolov, B. (2018). Hybrid Fuzzy-Probabilistic Approach to Supply Chain Resilience Assessment. IEEE Transactions on Engineering Management, 65(2), pp. 303-315.

Kirilin, A. N., Akhmetov, R. N., Shakhmatov, E. V., Tkachenko, S. I., Baklanov, A. I., Salmin, V. V., Semkin, N. D., Tkachenko, I. S., Goryachkin, O. V. (2017). Experimental and technological small spacecraft "AIST-2D". Samara: Publishing house of SamSC RAS, pp. 324.

Shipov, M. G. (2019). Damping of angular velocities of the Aist-2D spacecraft using the kinetic momentum release system. Bulletin of Samara University. Aviation and rocket-space technology 2(18), 121-127.

Mehdi Jafari (2015). Optimal redundant sensor configuration for accuracy increasing in space inertial navigation system // Aerospace Science and Technology, vol. 47. pp. 467–472.

Zavedeev, A. I. (1999). Development of algorithms for fault-tolerant control systems for aerospace aircraft. Proceedings of the VIII-th international scientific and technical seminar "Modern technologies in problems of control, automation and information processing". Alushta: Publishing house MAI, pp. 344-345.