1. A. I. Ignatov and V. V. Sazonov, “Realization of modes of satellite attitude motion with a small level of microaccelerations using electromechanical executive devices,” Cosmic Res. 50, 353 (2012).
2. L. A. Latyshev, A. F. Shtyrlin, O. M. Nepeivoda, and V. V. Sazonov, “The use of electric propulsions for realization of the motion of the satellite with low microgravity environment,” KIAM Preprint No. 16 (Keldysh Inst. Appl. Math., Moscow, 2007).
3. V. I. Abrashkin, Yu. A. Puzin, and V. V. Sazonov, “Electromagnetic attitude control system providing small residual accelerations on board the spacecraft,” KIAM Preprint No. 22 (Keldysh Inst. Appl. Math., Moscow, 2010).
4. A. I. Ignatov and V. V. Sazonov, “Stabilization of the spacecraft in the gravity gradient orientation mode by electromagnetic attitude control system,” KIAM Preprint No. 28 (Keldysh Inst. Appl. Math., Moscow, 2016).
5. A. I. Ignatov and V. V. Sazonov, “Realization of spacecraft attitude motion with small residual accelerations by electromechanical actuators,” KIAM Preprint No. 91 (Keldysh Inst. Appl. Math., Moscow, 2008).