Features of parametric synthesis of piecewise continuous programs of the pitch angle of the spacecraft on the active part of the trajectory taking into account the time pauses between the operation of the propulsion systems of its stages
The article considers an approach to choosing the optimal pitch angle trajectory for the stages of a space aircraft that provide the construction of a reference piecewise continuous flight path of the. A mathematical model of the stage movement under the action of forces in a uniform gravitational field at the time pause section in the earths coordinate system is presented.