Aerospace Instrument-Making Annotation << Back Adaptive correction inertial system orientation radio telescope Egorov Yu.G. Smirnov S.V. -The paper discusses the main issues of creating an autonomous precision -tion and con-tinuous functioning of the system for a long time error correction azimuthal orientation and identification tools for error of triaxial gyro inertial orientation of the radio telescope. Described functional scheme of work is presented a mathematical model and the results of theoretical studies of errors of estimating the parameters of the adaptive correction system. Shows the subdivision of the path of movement gyroplatform on the field for the synthesis of closed - circuit we estimation and identification of system parameters on the entire trajectory of motion of the gyro platform. The results of mathematical modeling of the adaptive correction system. Key words: correction system, system orientation radiotelescope gyroplatform. Contacts: E-mail: egoroviu2@yandex.ru Pp. 05-10.