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

Author:

Reshmin S. A.

Publisher

Pleiades Publishing Ltd

Subject

General Physics and Astronomy,Mechanics of Materials,Computational Mechanics

Reference15 articles.

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

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

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).

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).

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).

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