Estimation of the form of a large-sized transformed reflector surface for a spacecraft

This article offers a methodology of estimation of a spacecraft large-sized transformable reflector surface form, which allows to define the basic geometrical characteristics of the reflector, such as the focal point deflection and the focal axis deflection, zoom effect of paraboloid of the best fit for a deformable reflector surface, as well as the mean-squared deviation of the points which circumscribe the reflector surface.