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Using adaptation methods to stabilize elastic oscillations of large variable-parameter satellites

  • Robust and Adaptive Systems
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Abstract

Consideration was given to providing stability and some performance indices,—in particular, the transient time at reorientation—of the dynamics of large flexible-structure information satellites under a varying spectrum of its natural frequencies. A generalized system structure including the loop of adaptively adjusted additional feedback (AAF) was considered with the aim of providing the desirable system dynamics in the cases where the lower frequency approaches that of control of the “rigid” spacecraft motion. A procedure was presented to design an algorithm for adaptation of the coefficients of the AAF subsystem realizing the desirable dynamics of control of the large elastic satellites. The results of mathematical modeling corroborating efficiency of the proposed system were given.

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References

  1. Rutkovskii, V.Yu. and Sukhanov, V.M., On Stability of the Relay Control Systems of Flexible Satellite Orientation, Proc. IV Int. IFAC Symp. on Automatic Control in Space. Control in Space, Moscow: Nauka, 1973, vol. 1, pp. 37–43.

    Google Scholar 

  2. Somov, Ye.I., Butyrin, S.A., and Somov, S.Ye., Spacecraft Guidance and Robust Attitude Control with Precise Pointing the Flexible Antennas, Proc. 18th IEEE Int. Conf. Control Applications, part 3: IEEE Multi-conference on Systems and Control, St. Petersburg, 2009, pp. 1057–1062.

  3. Dodds, S.J., Adaptive Near-Time Optimal Control of Flexible Space Structures with a Discrete-Time on-line Parameter Estimator, Dynamics and Control of Structures in Space, IV, Kirk, C.L. and Vignjevic, R., Eds., Cranfield: Cranfield Univ., 1999, pp. 3–33.

    Google Scholar 

  4. Kabganian, M. and Shahravi, M., Attitude Tracing and Vibration of Flexible Spacecraft Using Implicit Adaptive Control Law, Proc. 16 IFAC Symp. Automat. Control Aerospace, 2004, vol. 1, pp. 91–97.

    Google Scholar 

  5. Rutkovsky, V.Yu., Zemlyakov, S.D., Sukhanov, V.M., and Glumov, V.M., Modeling and Adaptive Attitude Control of Observation Spacecraft in View of Flexible Structure, 17th Congress IFAC, Seoul, 2008, pp. 3440–3445.

  6. Glumov, V.M., Krutova, I.N., and Sukhanov, V.M., Fuzzy Logic-based Adaptive Control System for Inorbit Assembly of Large Space Structures, Autom. Remote Control, 2004, vol. 65, no. 10, pp. 1618–1634.

    Article  MATH  MathSciNet  Google Scholar 

  7. Krutova, I.N. and Sukhanov, V.M., Design of Modified PD Algorithm to Control Angular Motion of Large Space Structure, Autom. Remote Control, 2009, vol. 70, no. 1, pp. 33–42.

    Article  MATH  MathSciNet  Google Scholar 

  8. Nurre, G.S., Ryan, R.S., Skofield, H.N., and Sims, J.I., Dynamics and Control of Large Space Structures, Aerokosm. Tekhn., 1985, vol. 3, no. 6, pp. 71–80.

    Google Scholar 

  9. Glumov, V.M., Zemlyakov, S.D., Rutkovskii, V.Yu., and Sukhanov, V.M., Spatial Angular Motion of a Flexible Spacecraft: The Modal-Physical Model and Its Characteristics, Autom. Remote Control, 1998, vol. 59, no. 12, part 1, pp. 1728–1738.

    MATH  Google Scholar 

  10. Raushenbakh, B.V. and Tokar’, E.N., Upravlenie orientatsiei kosmicheskikh apparatov (Control of Spacecraft Orientation), Moscow: Nauka, 1974.

    Google Scholar 

  11. Glumov, V.M., Rutkovskii, V.Yu., and Sukhanov, V.M., Adaptive Control of Orientation of Flexible Spacecraft with Variable Parameters, Autom. Remote Control, 1999, vol. 60, no. 4, part 2, pp. 564–574.

    Google Scholar 

  12. Glumov, V.M., Rutkovskii, V.Yu., and Sukhanov, V.M., Methods of Intelligent Diagnosis for Control of Flexible Moving Craft, Autom. Remote Control, 2006, vol. 67, no. 12, pp. 1863–1877.

    Article  MATH  MathSciNet  Google Scholar 

  13. Borisov, B.G., Ermilov, A.S, Ermilova, T.V., and Sukhanov, V.M., Joint Estimation and Identification in the Discrete Control Systems of the Flexible Spacecraft, in Second Int. Conf. “System Identification and Control Problems” (SICPRO’ 03), Moscow: Inst. Probl. Upravlen., 2003, pp. 2278–2284.

    Google Scholar 

  14. Voronov, A.A., Osnovy teorii avtomaticheskogo upravleniya. Chast’ 1 (Fundamentals of the Automatic Control Theory. Part 1), Moscow: Energiya, 1965.

    Google Scholar 

  15. Zemlyakov, S.D. and Rutkovskii, V.Yu., Algorithm of Precise Control of a Dynamic Object under Uncertainty Based on the Adaptive System with Reference Model, Dokl. Ross. Akad. Nauk, 2009, vol. 429, no. 2, pp. 176–179.

    MathSciNet  Google Scholar 

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Authors and Affiliations

  1. Trapeznikov Institute of Control Sciences, Russian Academy of Sciences, Moscow, Russia

    V. Yu. Rutkovskii, V. M. Sukhanov & V. M. Glumov

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  1. V. Yu. Rutkovskii
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  2. V. M. Sukhanov
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  3. V. M. Glumov
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Original Russian Text © V.Yu. Rutkovskii, V.M. Sukhanov, V.M. Glumov, 2011, published in Avtomatika i Telemekhanika, 2011, No. 12, pp. 91–103.

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Rutkovskii, V.Y., Sukhanov, V.M. & Glumov, V.M. Using adaptation methods to stabilize elastic oscillations of large variable-parameter satellites. Autom Remote Control 72, 2505–2515 (2011). https://doi.org/10.1134/S000511791112006X

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  • DOI: https://doi.org/10.1134/S000511791112006X

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