2015
DOI: 10.3390/s150923684
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Error Model and Compensation of Bell-Shaped Vibratory Gyro

Abstract: A bell-shaped vibratory angular velocity gyro (BVG), inspired by the Chinese traditional bell, is a type of axisymmetric shell resonator gyroscope. This paper focuses on development of an error model and compensation of the BVG. A dynamic equation is firstly established, based on a study of the BVG working mechanism. This equation is then used to evaluate the relationship between the angular rate output signal and bell-shaped resonator character, analyze the influence of the main error sources and set up an er… Show more

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Cited by 5 publications
(2 citation statements)
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“…In Figure 1 b, radial velocity is introduced in addition to the relative circumferential velocity between the conducting fluid and rotating case. At low rotating frequency, relative circumferential velocity is weakened by the viscous and electromagnetic force but accelerated due to Coriolis acceleration similar to other Coriolis vibratory gyroscopes [ 33 , 34 ] and then a radially-oriented electric field is generated, whereas the MHD effects illustrated in the basic MHD ARS dominate at high frequency. The measurement through the whole bandwidth is achieved by combing the Coriolis effect at low frequency and MHD effect at high frequency.…”
Section: Simplified Model Of Modified Mhd Arsmentioning
confidence: 93%
“…In Figure 1 b, radial velocity is introduced in addition to the relative circumferential velocity between the conducting fluid and rotating case. At low rotating frequency, relative circumferential velocity is weakened by the viscous and electromagnetic force but accelerated due to Coriolis acceleration similar to other Coriolis vibratory gyroscopes [ 33 , 34 ] and then a radially-oriented electric field is generated, whereas the MHD effects illustrated in the basic MHD ARS dominate at high frequency. The measurement through the whole bandwidth is achieved by combing the Coriolis effect at low frequency and MHD effect at high frequency.…”
Section: Simplified Model Of Modified Mhd Arsmentioning
confidence: 93%
“…In summary, the errors of IMU inertial devices can be divided into four categories: zero-position error, scale factor error, cross-coupling error, and random error. In the process of pedestrian heading attitude calculation, the accuracy and stability of gyro output play a more critical role (the stability is relatively poor, and it is easy to be interfered by external environment and its own device characteristics) [19]. Therefore, this section focuses on the gyro calibration description.…”
Section: Inertial Data Preprocessing a The Compensation Calibrationmentioning
confidence: 99%