1. V. N. Branets and I. P. Shmyglevskii, Application of Quaternions to Rigid Body Attitude Problems (Nauka, Moscow, 1973) [in Russian].
2. M. V. Levskii, “The use of universal variables in problems of optimal control of the orientation of spacecraft,” Mekhatron. Automat. Uprav., No. 1, 53–59 (2014).
3. K. B. Alekseev, A. A. Malyavin, and A. V. Shadyan, “Spacecraft extensive attitude control based on fuzzy logic,” Polet, No. 1, 47 (2009).
4. O. V. Ermoshina and A. P. Krishchenko, “Synthesis of programmed controls of spacecraft orientation by the method of inverse problem of dynamics,” J. Comput. Sys. Sci. Int. 39 (2), 313–320 (2000).
5. M. A. Velishchanskii, A. P. Krishchenko, and S. B. Tkachev, “Synthesis of spacecraft reorientation algorithms using the concept of the inverse dynamic problem,” J. Comput. Syst. Sci. Int. 42, 811 (2003).