The impact of lifting the meridian line of the suspension on the accuracy of the inertial sensor
DOI:
https://doi.org/10.15587/1729-4061.2014.21870Keywords:
systematic inaccuracy, inertial sensor, meridian line, middle frame, gyro suspensionAbstract
Numerical analysis of the effectiveness of reducing the impact of a shock N-wave of hypersonic flight using the methods of design and technology solutions is carried out. In particular, through the transition from surfaces with non-zero Gaussian curvature of the moving part of float suspension of two-stage inertial sensor to surfaces with non-zero Gaussian curvature. Technical realization of this transition lies in an artificial lifting the meridian line of float by the value in the middle frame. Elastically deformed surface of float suspension in the case of cyclic loading by diffuse sound field with intensity and frequency is presented. Numerical values of maximum elastic displacements of the suspension surface in the middle frame of the moving part of a commercially available device are given, and the systematic inaccuracy of sensor for several variants of lifting the meridian line of the float is determined. In particular, lifting the meridian line of the middle frame by the value of (1,7÷1,8)10-3 m allows to provide the systematic inaccuracy of the device in the acoustic field at the level of its sensitivity threshold, i.e. not higher than 0.45 deg c-1. Results can be used for testing prototypes and assessing the compliance of operating devices with the passport requirements.
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