Aerospace Instrument-Making Annotation << Back BIAXIAL INDICATOR FLYWHEEL GYROSTABILIZER A.V. Kuleshov, V.P. Podchezertsev, V.V. Fateev, D.A. Bordachev The article discusses the features of the construction of a biaxial flywheel indicator gyrostabilizer with unloading by angular rate of the flywheel. The special attention is paid to research the influence of gyroscopic and damping cross linking about the axes of stabilization, shows their small effect on the stability and accuracy of the gyrostabilizer. The paper presents the equations of motion of a biaxial flywheel gyrostabilizer, received full expression for the gyrostabilizer angles about stabilization axes, defined steady stabilization angle and steady speed of the flywheel rotation when exposed constant torque of external forces on gyrostabilizer. Key words: indicator gyrostabilizer, powered gyrostabilizer, biaxial gyrostabilizer, flywheel, the unloading system. Contacts: E-mail: akul1974@mail.ru Pp. 03-12.