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Roll control of a flight vehicle with the adjustable center of mass

  • Flight Dynamics and Control of Flight Vehicles
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Abstract

We present the results of analytical research of flight dynamics for a flight vehicle that is controlled by the adjustable center of mass in the vertical symmetry plane. The roll oscillations, which appear perpendicular to the symmetry plane due to technological errors, are eliminated by means of control rocket engines, for which a control law is assigned.

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References

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Authors and Affiliations

  1. South Ural State University (National Research University), pr. Oktyabrya 16, Miass, 456318, Russia

    V. A. Afanas’ev & V. I. Kiselev

  2. Tupolev Kazan National Research Technical University, ul. Karla Marksa 10, Kazan, Tatarstan, 420111, Russia

    G. L. Degtyarev & A. S. Meshchanov

Authors
  1. V. A. Afanas’ev
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  2. G. L. Degtyarev
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  3. V. I. Kiselev
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  4. A. S. Meshchanov
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Corresponding author

Correspondence to V. A. Afanas’ev.

Additional information

Original Russian Text © V.A. Afanas’ev, G.L. Degtyarev, V.I. Kiselev, and A.S. Meshchanov, 2017, published in Izvestiya Vysshikh Uchebnykh Zavedenii, Aviatsionnaya Tekhnika, 2017, No. 1, pp. 48–54.

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Afanas’ev, V.A., Degtyarev, G.L., Kiselev, V.I. et al. Roll control of a flight vehicle with the adjustable center of mass. Russ. Aeronaut. 60, 50–56 (2017). https://doi.org/10.3103/S1068799817010081

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  • DOI: https://doi.org/10.3103/S1068799817010081

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