Aerospace Instrument-Making Annotation << Back The application of reconfiguration principal to design the tollerant majority flight control computing system N.N. Sukhikh, A.G. Kovalev, V.L. Rukavishnikov This method is designed to provide the efficiency of majority computing system after two consecutive computer failures are happened. The creation of this system is based on using the part time control regulator. Key words: efficiency of majority computing system, systems of automatic flight management, failure-resistance E-mail: valentine_lr@mail.ru