Estimate of the control threshold value in the problem on a time-optimal satellite attitude transition maneuver

Author:

Reshmin S. A.

Publisher

Allerton Press

Subject

General Physics and Astronomy,Mechanics of Materials

Reference12 articles.

1. V. V. Beletskii, “Optimal Transfer of an Earth Satellite to a Gravitationally Stable Position,” Kosmich. Isseld. 9 (3), 366–375 (1971) [Cosmic Res. (Engl. Transl.) 9 (3), 337–344 (1971)].

2. A. A. Anchev, “Equilibrium Attitude Transitions of a Three-Rotor Gyrostat in a Circular Orbit,” AIAA J. 11 (4), 467–472 (1973).

3. A. P. Markeev, Theoretical Mechanics (NITs “Regular and Chaotic Dynamics,” Moscow–Izhevsk, 2007) [in Russian].

4. S. A. Reshmin and F. L. Chernous’ko, “A Time-Optimal Control Synthesis for a Nonlinear Pendulum,” Izv. Ross. Akad. Nauk. Teor. Sist. Upr., No. 1, 13–22 (2007) [J. Comp. Syst. Sci. Int. (Engl. Transl.) 46 (1), 9–18 (2007)].

5. S. A. Reshmin, “Finding the Principal Bifurcation Value of the Maximum Control Torque in the Problem of Optimal Control Synthesis for a Pendulum,” Izv. Ross. Akad. Nauk. Teor. Sist. Upr., No. 2, 5–20 (2008) [J. Comp. Syst. Sci. Int. (Engl. Transl.) 47 (2), 163–178 (2008)].

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