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Control of a Piezo Actuator to Adjust the Reflective Surface of the Space-Based Reflector

  • Radio Engineering and Communication
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Abstract

The task of adjusting and maintaining the shape of the radio-reflective network of a largesized space-based reflector is considered. The possibility of using piezo actuators to solve this problem is estimated. The urgency of the actuator control problem for a wide range of tasks related to the space and aircraft equipment is shown. Different types of control for the chosen mathematical model of a piezo actuator are compared.

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Authors and Affiliations

  1. Ustinov Baltic State Technical University “Voenmekh”, ul. 1ya Krasnoarmeiskaya 1, St. Petersburg, 190005, Russia

    S. A. Kabanov, F. V. Mitin & A. I. Krivushov

  2. Reshetnev AO ISS, ul. Lenina 52, Zheleznogorsk, Krasnoyarskii krai, 662972, Russia

    E. A. Ulybushev

Authors
  1. S. A. Kabanov
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  2. F. V. Mitin
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  3. A. I. Krivushov
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  4. E. A. Ulybushev
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Corresponding author

Correspondence to F. V. Mitin.

Additional information

Original Russian Text © S.A. Kabanov, F.V. Mitin, A.I. Krivushov, E.A. Ulybushev, 2018, published in Izvestiya Vysshikh Uchebnykh Zavedenii, Aviatsionnaya Tekhnika, 2018, No. 4, pp. 111–116.

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Kabanov, S.A., Mitin, F.V., Krivushov, A.I. et al. Control of a Piezo Actuator to Adjust the Reflective Surface of the Space-Based Reflector. Russ. Aeronaut. 61, 629–635 (2018). https://doi.org/10.3103/S1068799818040189

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  • DOI: https://doi.org/10.3103/S1068799818040189

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