Aerospace Instrument-Making Annotation << Back Utilization of on-board standard system of three gyroscopic integrators of linear accelerations integrated into gyroscopic complex of control devices in order to measure linear acceleration vector of load-bearing apparatus I.Ya. Ogurtsov On the basis of complete differential equations of movement of gyroscopic integrator construction of linear accelerations with elemental interframe correcting system a mathematic model of standard block of gyro integrators of gyroscopic complex was developed in order to measure vectors of absolute linear acceleration on location. It was also developed to obtain actual measuring of angular velocity of the device’s location on the gyro stabilized platform. There are two variants of the model: an algebraical and a frequency one. Impact resistance of the gyro integrator construction performed in a classic form of gyro pendulum was studied and its principle invalidity was shown. Mechanical properties of gyro integrator as identifiers of impact forces were closely examined. Key words: Differential equations, gyroscopic integrator, linear accelerations, interframe correcting system, vectors of linear acceleration, gyro stabilized platform, identification. E-mail: pahik@mail.ru