1. Branets, V.N. and Shmyglevskii, I.P., Primenenie kvaternionov v zadachakh orientatsii tverdogo tela (Quaternions Application for Problems on Orientation of Rigid Body), Moscow: Nauka, 1973.
2. Alekseev, K.B. and Bebenin, G.G., Upravlenie kosmicheskimi letatel’nymi apparatami (Control for Spacecrafts), Moscow: Mashinostroenie, 1974.
3. Branets, V.N., Chertok, M.B., and Kaznacheev, Yu.V., Optimal turn of rigid body with one axis of symmetry, Kosm. Issled., 1984, vol. 22, no. 3, pp. 352–360.
4. Li, F. and Bainum, P.M., Numerical approach for solving rigid spacecraft minimum time attitude maneuvers, J. Guid., Control, Dyn., 1990, vol. 13, no. 1, pp. 38–45.
5. Scrivener, S. and Thompson, R., Survey of time-optimal attitude maneuvers, J. Guid., Control, Dyn., 1994, vol. 17, no. 2, pp. 225–233.