A MEMS-Based Rate Gyro Based on Parametric Resonance

Author(s):  
Nicholas J. Miller ◽  
Steven W. Shaw ◽  
Laura A. Oropeza-Ramos ◽  
Kimberly L. Turner

This paper describes the dynamics of a microelectromechanical rate gyro whose operation depends on nonlinear parametric resonant response. The basic idea behind this and other similar gyros is that a proof mass is free to move in a plane such that the perpendicular directions of motion are ideally mechanically uncoupled. In one direction, the drive mode, the mass is parametrically driven such that it undergoes a nonlinear resonant response. When rotated about an axis perpendicular to the plane of motion, Coriolis effects couple this drive mode to the other direction, the sense mode, whose response is then measured and calibrated with the rotation rate. Traditional rate gyros of this type require precise matching of the drive and sense linear natural frequencies in order to optimally amplify the sense response. By making use of the wide frequency range of the nonlinear resonant response, many of the difficulties associated with this tuning problem can be avoided. In this paper we emphasize results from a simple two degree-of-freedom micro-electro-mechanical system model that allows one to predict and design the rate response of the gyro by selection of system parameters.

1980 ◽  
Vol 47 (1) ◽  
pp. 161-166 ◽  
Author(s):  
C. H. J. Fox ◽  
J. S. Burdess

This study investigates the dynamics of a gyroscope rotor, supported on a “heavy” elastic suspension, using a mathematical model which allows the gyroscope to be treated as a two-degree-of-freedom rigid body on a light suspension. The natural frequencies are functions of spin rate and it is shown that the lower natural frequency can be reduced to zero by appropriate selection of suspension parameters. In this condition the gyroscope is “tuned” and could provide a useful inertial reference. Some problems associated with predicting the tuning speed of a practical gyroscope are highlighted.


2021 ◽  
Vol 332 ◽  
pp. 113129
Author(s):  
Ara Yeon ◽  
Hong Goo Yeo ◽  
Yongrae Roh ◽  
Kyungseop Kim ◽  
Hee-Seon Seo ◽  
...  

2000 ◽  
Author(s):  
Paul B. Deignan ◽  
Peter H. Meckl ◽  
Matthew A. Franchek ◽  
Salim A. Jaliwala ◽  
George G. Zhu

Abstract A methodology for the intelligent, model-independent selection of an appropriate set of input signals for the system identification of an unknown process is demonstrated. In modeling this process, it is shown that the terms of a simple nonlinear polynomial model may also be determined through the analysis of the average mutual information between inputs and the output. Average mutual information can be thought of as a nonlinear correlation coefficient and can be calculated from input/output data alone. The methodology described here is especially applicable to the development of virtual sensors.


Author(s):  
R. J. Henderson ◽  
J. K. Raine

Parts 1 and 2 of this paper gave a design overview and described the dynamics of a prototype two-degree-of-freedom pneumatic suspension for an ambulance stretcher. This concluding part briefly reviews laboratory shaker table and ambulance road test performance of the suspension with passive pneumatic damping. The suspension system is found to offer compact low-cost isolation with lower natural frequencies than achieved in earlier mechanical systems.


1999 ◽  
Vol 103 (1020) ◽  
pp. 95-103 ◽  
Author(s):  
W. R. Graham

Abstract A new approach to deriving analytical approximations for the free modes of motion of an aircraft is presented. Based on an asymptotic analysis, it eliminates the need for a priori assumptions regarding the characteristic motion of each mode, and is thus particularly suitable for an introductory exposition. In its basic form, it yields expressions for natural frequencies, damping factors and time constants which agree, to leading order, with well established results. At a more advanced level, it allows us to assess the validity of these results. In particular, we find that the two degree-of-freedom approximations to the short period oscillation and Dutch roll are asymptotically incorrect. This is unlikely to have a significant effect on the accuracy of the former, but is the reason for the poor damping predictions of the latter.


Sign in / Sign up

Export Citation Format

Share Document