1. Mkrtychyan, A.R., Bashkeev, N.I., Akashev, D.I., Andryushin, E.O., Konoplev, A.V., and Chudakov, V.V., Some issues of designing CMG systems for attitude control systems of small sized remote sensing satellites, 4th Scientific and technical conference “Aktual’nye problemy sozdaniya kosmicheskikh sistem distantsionnogo zondirovaniya Zemli” (Relevant Problems in Earth Remote Sensing Systems), Moscow: VNIIEM Corporation, 2016, pp. 120–124.
2. Sorokin, A.V. and Bashkeev, N.I., Comparative analysis of the power gyroscopic complexes for the agile satellites, 10
th
St. Petersburg International Conference on Integrated Navigation Systems, 2003, pp. 272–277.
3. Mkrtychyan, A.R., Bashkeev, N.I., Yakimovskii, D.O., Akashev, D.I., and Yakovets, O.B., Control-moment gyroscope systems for spacecraft: Current status and prospects, Gyroscopy and Navigation, 2015, vol. 6, no. 3. https://doi.org/10.1134/S2075108715030116
4. Levskii, M.V., On improving the maneuverability of a space vehicle managed by inertial executive bodies, Journal of Computer and Systems Sciences International, vol. 59, no. 5. https://doi.org/10.1134/S1064230720020094
5. Uglova, A.O. and Luk’yanenko, M.V., Estimating the advantages of using control moment gyros in spacecraft attitude control and stabilization systems, Proceedings of the 5th International Scientific and Practical Conference “Aktual’nye problem aviatsii i kosmonavtiki” (Relevant Issues in Aviation and Space Industry), Loginov, Yu.Yu., Ed., Krasnoyarsk: Reshetnev Siberian State University of Science and Technology, 2019, vol. 1, pp. 601–603.