Aerospace Instrument-Making Annotation << Back Method of analytical solutions in simulation and designing of the control systems for returned space vehicles V.A. Afanasjev, N.N. Malivanov, A.S. Meshchanov Analytical solutions have been obtained for differential equations describing angular motion into atmosphere that permit us to simulate the control system of return space vehicles during angular turns and oscillation damping. The results are used for complex designing of the space vehicle together with its control system as well as for development of onboard control system.