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Modeling of the Deployment Process Dynamics for Large-Sized Transformable Space Structures

  • FLIGHT DYNAMICS AND CONTROL OF FLIGHT VEHICLES
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Abstract

A dynamic model of the deployment of the large-sized transformable space structures (by the example of solar panels) is proposed. The model is based on using the Lagrange equations of the second kind. The model capabilities are illustrated by calculation results of the main integral parameters characterizing the solar panel deployment process.

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ACKNOWLEDGEMENTS

The work was carried out within the framework of the state assignment, the number of state registration of the topic AAAA-A19-119012290177-0.

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Authors and Affiliations

  1. Institute of Applied Mechanics, Russian Academy of Sciences, pr. Leningradskii 7, 125040, Moscow, Russia

    V. N. Bakulin

  2. PAO S.P. Korolev Rocket and Space Corporation Energiya, ul. Lenina 4A, 662972, Korolev, Moscow oblast, Russia

    S. V. Borzykh

Authors
  1. V. N. Bakulin
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  2. S. V. Borzykh
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Corresponding author

Correspondence to V. N. Bakulin.

Additional information

Translated from Izvestiya Vysshikh Uchebnykh Zavedenii, Aviatsionnaya Tekhnika, 2020, No. 4, pp. 50 - 56.

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Bakulin, V.N., Borzykh, S.V. Modeling of the Deployment Process Dynamics for Large-Sized Transformable Space Structures. Russ. Aeronaut. 63, 610–617 (2020). https://doi.org/10.3103/S1068799820040078

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  • DOI: https://doi.org/10.3103/S1068799820040078

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