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The Threshold Absolute Value of a Relay Control Bringing a Satellite to a Gravitationally Stable Position in Optimal Time

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Abstract

The properties of the solution to the well-known problem of the optimal orientation of a satellite in the plane of a circular orbit and its steering to a gravitationally stable angular position, which was posed and considered earlier by Vladimir V. Beletskij, have been refined. The constraint on the control torque module is considered as the main parameter of the problem. It turned out that, even in the case when the admissible control torque exceeds the gravitational moment in magnitude, in the phase plane the existence of additional switching curves corresponding to relay control with two switchings is possible. As a result, a simple numerical algorithm is proposed, and with its help the threshold absolute control value is found at which the indicated switching curves are infinitesimal, and their coordinates in the phase plane are found.

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References

  1. V. V. Beletskij, On Optimal Guiding of an Artificial Earth Satellite into a Gravitationally Stable Attitude, Cosmic Res. 9 (3), 337 (1971).

    Google Scholar 

  2. B. Friedland and P. Sarachik, Indifference Regions in Optimum Attitude Control, IEEE Trans. Automatic Control 9 (2), 180 (1964).

    Article  Google Scholar 

  3. Chernousko F.L., Optimal Control of Two-Dimensional Motions of a Body by a Movable Mass, Proc. 9th Vienna International Conference on Mathematical Modelling. 21–23 February (2018); IFAC-PapersOnLine 51 (2), 232 (2018).

    Google Scholar 

  4. A. N. Sirotin. A Family of Trigonometric Extremals in the Problem of Reorienting a Spherically Symmetrical Body with Minimum Energy Consumption. J. Appl. Mat. Mech. 77 (2), 205 (2013).

    Google Scholar 

  5. M. V. Levskii, Analytic Controlling Reorientation of a Spacecraft Using a Combined Criterion of Optimality. J. Comp. Syst. Sci. Int. 57 (2), 283 (2018).

    Google Scholar 

  6. V. S. Aslanov and S. P. Bezglasnyi, Gravitational Stabilization of a Satellite Using a Movable Mass. J. Appl. Math. Mech. 76 (4), 405 (2012).

    Google Scholar 

  7. S. P. Bezglasnyi and A. A. Mukhametzyanova, Gravitational Stabilization and Reorientation of a Satellite- Dumbbell in the Circular Orbit under the Swing Principles, Avtomatizatsiya Protsessov Upravleniya, No. 1 (43), 91 (2016).

    Google Scholar 

  8. A. P. Markeev, Theoretical Mechanics (NITs “Regular and Chaotic Dynamics”, Moscow–Izhevsk, 2007).

    Google Scholar 

  9. S. A. Reshmin, Bifurcation in a Time-Optimal Problem for a Second-Order Non-Linear System. J. Appl. Math. Mech. 73 (4), 403 (2009).

    MathSciNet  Google Scholar 

  10. S. A. Reshmin, Dispersal Curve Properties in the Time Minimization Problem for a Second-Order Nonlinear System. J. Comp. Syst. Sci. Int. 51 (3), 366 (2012).

    MathSciNet  Google Scholar 

  11. S. A. Reshmin and F. L. Chernousko, Properties of the Time-Optimal Feedback Control for a Pendulum-Like System. J. Optimiz. Theory Appl. 163 (1), 320 (2014).

    Google Scholar 

  12. S. A. Reshmin, Estimate of the Control Threshold Value in the Problem on a Time-Optimal Satellite Attitude Transition Maneuver, Mech. Solids 52 (1), 9 (2017).

    MathSciNet  Google Scholar 

  13. E. B. Lee and L. Markus, Foundations of Optimal Control Theory (Wiley, New York, 1967; Nauka, Moscow, 1972).

    Google Scholar 

  14. J. L. Garcia Almuzara and I. Flügge-Lotz, Minimum Time Control of a Nonlinear System. J. Differen. Equats 4 (1), 12 (1968).

    Google Scholar 

  15. S. A. Reshmin, Finding the Principal Bifurcation Value of the Maximum Control Torque in the Problem of Optimal Control Synthesis for a Pendulum. J. Comp. Syst. Sci. Int. 47 (2), 163 (2008).

    MathSciNet  Google Scholar 

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Correspondence to S. A. Reshmin.

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Original Russian Text © S.A. Reshmin, 2018, published in Doklady Akademii Nauk, 2018, Vol. 480, No. 6, pp. 671–675.

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Reshmin, S.A. The Threshold Absolute Value of a Relay Control Bringing a Satellite to a Gravitationally Stable Position in Optimal Time. Dokl. Phys. 63, 257–261 (2018). https://doi.org/10.1134/S1028335818060101

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  • DOI: https://doi.org/10.1134/S1028335818060101

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