1. El’yasberg, P.E., Vvedenie v teoriyu poleta iskusstvennykh sputnikov Zemli (Introduction to the Flight Theory of Man-Made Earth Satellites), Moscow: Nauka, 1965.
2. Grodzovskii, G.L., Ivanov, Yu.N., and Tokarev, V.V., Mekhanika kosmicheskogo poleta. Problemy optimizatsii (Space Flight Mechanics. Optimization Problems), Moscow: Nauka, 1975.
3. Okhotsimskii, D.E. and Sikharulidze, Yu.G., Osnovy mekhaniki kosmicheskogo poleta (Fundamentals of Space Flight Mechanics), Moscow: Nauka, 1990.
4. Grigorev, I.S. and Grigorev, K.G., Conditions of the Maximum Principle in the Problem of Optimal Control over an Aggregate of Dynamic Systems and Their Application to Solution of the Problems of Optimal Control of Spacecraft Motion, Kosm. Issled., 2003, vol. 41, no. 3, pp. 307–331.
5. Grigor’ev, I.S. and Danilina, I.A., Optimization of Interorbital Three-dimensional Transfer Trajectories for Stage Spacecraft, Autom. Remote Control, 2007, vol. 68, no. 8, pp. 1372–1390.