Aerospace Instrument-Making Annotation << Back FLYWHEEL INDICATOR GYROSTABILIZER WITH UNLOADING TO A FLYWHEEL A.V. Kuleshov, V.V. Fateev, E.S. Tverskaya The article discusses the construction of an indicator flywheel gyrostabilizer with unloading by the rotational speed of the flywheel. Herewith unloading may be effected by applying a torque to the platform of gyrostabilizer or to the flywheel itself. In the first case it is possible to significantly improve the accuracy of the stabilization, but such principle of organizing the unloading requires the mounting of additional drive and the measuring system of the flywheel speed that creates the additional constructive complexity. In the second case, a constructive solution of gyrostabilizer is considerably simpler and unloading may be accomplished using aerodynamic, hydrodynamic, gravitational, magnetic or other forces. This article discusses the flywheel gyrostabilizer with aerodynamic unloading. The mathematical model of gyrostabilizer and results of studies of its stability, accuracy, and quality control are represented. Key words: indicator gyrostabilizer, flywheel, flywheel gyrostabilizer, the unloading system. Contacts: E-mail: akul1974@mail.ru Pp. 03-10.