Предложена реализация информациионной технологии проведения аэродинамических испытаний. Разработана структурная, функциональная схема измерительного канала, произведен расчет погрешностей и предложен метод их уменьшения путем тройного экранирования. Разработано прикладное ПО на языке assembler.
Realization of information technology of aerodynamic tests conducting has been suggested. Structural, functional schemes of measuring system channel have been developed, errors calculation has been made and the way of their reduction by means of triple screening has been suggested. Application software on the assembler language has been developed.