Kalinina M. Wave processes in suspension of gyroscopes and motion control problems of hypersonic vehicles

Exposed nature of origin of additional errors of gyroscopic integrator of linear accelerations during flying exploitation, analytically described influence of cross axes of hanging of gyroscope and diffraction phenomena under the action of penetrating acoustic radiation, that form in material nonlinear vibrations and create the resiliently-tense state to the same, by received device for useful. Constructed calculation model and created dynamics of torsion suspend of gyroscope software are on the basis of wave equalization. The outlined terms of origin of the "acoustic-transparent" state of element base are in the diffuse field. The well-proven efficiency of last of cyclic quadratic chain code is for a reflection a rotor siren in the surface terms of acoustic situation of hyper sound flight. Some practical aspects of pre-flight attestation of gyroscopes that are in composition of aircrafts on open starting positions are exposed.