1. Anshakov, G. P., Antonov, Yu. G., Butyrin, S. A., Makarov, V. P., Matrosov, V. M., & Somov, Ye. I. (1995). Gyromoment attitude control systems dynamics of rapid manoeuvring remote sensing spacecraft. Proceedings of the first international aerospace congress, vol. 2 (pp. 129-132). Moscow: Petrovka.
2. Aref'yev, V. P., Sorikin, A. V., Bashkeyev, N. I., & Kondrat'yev, O. A. (1995). Gyrotorque devices of spacecraft attitude systems. Gyro-techniques and navigation, (2), 7–11.
3. Bartenev, V. A., Malyshev, V. A., Rayevsky, V. A., Titov, G. P., & Somov, Ye. I. (1998). Orbit and attitude control systems of Russian communication, geogetic and navigation spacecraft. Preprints of the 14th symposium IFAC on automatic control in aerospace. (pp. 15–26). Seoul:SNU.
4. Hubble Space Telescope precision pointing control system;Beals;Journal of Guidance, Control, and Dynamics,1988
5. Crenshaw, J. W. (1973). 2-SPEED, a single-gimbal control moment gyro attitude control systems. AIAA Paper (73-895), 1–10.