A Stable Parametrically Amplified Gyroscope
Lead Research Organisation:
Newcastle University
Department Name: Mechanical and Systems Engineering
Abstract
Despite the huge industrial and academic effort in advancing both the precision of the fabrication, mass trimming and signal processing there is still a considerable amount of improvement required before MEMS gyroscopes challenge the performance of other gyroscopic technologies. The objective of the proposed research is to develop an excitation scheme to enable stable parametric amplification of the Q-factors of the sense and drive modes of vibration of a typical electrostatically driven MEMS gyroscope and thus improve gyroscopic performance by at least an order of magnitude. Parametric amplification reduces the amount of total damping (viscous and thermoelastic) present in a resonator and may be interpreted as amplification in the effective Q-factor or as force amplification. Mis-tuning between the important modes of vibration must be minimised in conventionally excited gyroscopes to realise high performance. By employing parametric excitation and amplification the degree of mis-tuning that can be tolerated is increased and will allow the affect of Q-factor amplification on the gyroscope performance to be maximised. Eradicating the need to precisely tune the modes is in itself an important development and when combined with the parametric amplification of the Q-factor the prospect of a step change in MEMS gyroscope performance is a distinct possibility. It has the potential to transform a gyroscope which is rate grade to tactical grade. This work is also very applicable to resonant MEMS/NEMS sensors in general where high Q-factors are essential for the sensor performance. We propose to establish the full extent of amplification possible via parametric action, its limiting factors and develop the scheme necessary to use it optimally in actual MEMS gyroscopes.
Publications
Bowles S
(2015)
Control Scheme to Reduce the Effect of Structural Imperfections in a Rate Integrating MEMS Gyroscope
in IEEE Sensors Journal
Bowles S
(2014)
Control scheme for a rate integrating MEMS gyroscope
Gallacher B
(2013)
The Application of Parametric Excitation in MEMS Gyroscopes
Gallacher B
(2014)
Applied Non-Linear Dynamical Systems
Gallacher B
(2012)
Principles of a Micro-Rate Integrating Ring Gyroscope
in IEEE Transactions on Aerospace and Electronic Systems
Gallacher B J
(2017)
non linear dynamics
Grigg H
(2012)
Efficient Parametric Optimisation of Support Loss in MEMS beam resonators via an enhanced Rayleigh-Ritz method
in Journal of Physics: Conference Series
Grigg H
(2014)
An efficient general approach to modal analysis of frame resonators with applications to support loss in microelectromechanical systems
in Journal of Sound and Vibration
Hu Z
(2016)
Extended Kalman filtering based parameter estimation and drift compensation for a MEMS rate integrating gyroscope
in Sensors and Actuators A: Physical
Hu Z
(2014)
A systematic approach for precision electrostatic mode tuning of a MEMS gyroscope
in Journal of Micromechanics and Microengineering
Description | Ways of sustaining vibration in Coriolis gyros. Methods of closed loop control over mode tuning. Full state (displacement and velocity) feedback for reducing errors. Damping compensation implemented. |
Exploitation Route | All resonant sensors rely on resonance. Thus mode tuning and Q-factor pumping can be used to improve sensor performance. |
Sectors | Aerospace Defence and Marine Electronics |
Description | Yes. We are collaborating with UTAS/ Goodrich on advanced gyro control based on the research findings |
First Year Of Impact | 2014 |
Sector | Aerospace, Defence and Marine |
Impact Types | Economic |
Description | Atlantic Inertial Systems Ltd |
Amount | £70,000 (GBP) |
Funding ID | rate integrating gyro |
Organisation | UTC Aerospace Systems |
Sector | Private |
Country | United States |
Start | 08/2011 |
End | 09/2014 |
Description | Atlantic Inertial Systems Ltd |
Amount | £70,000 (GBP) |
Funding ID | rate integrating gyro |
Organisation | UTC Aerospace Systems |
Sector | Private |
Country | United States |
Start | 08/2011 |
End | 09/2014 |
Description | Advanced Gyro control systems |
Organisation | United Technologies Research Center (UTRC) |
Country | United States |
Sector | Private |
PI Contribution | Gyro control system |
Collaborator Contribution | Provided devices |
Impact | Reports (Confidential) |
Start Year | 2014 |
Description | RATE INTEGRATING GYRO |
Organisation | Goodrich Corporation |
Country | United States |
Sector | Private |
PI Contribution | Supervised a PHD student. developed control strategies |
Collaborator Contribution | provided MEMS gyros. technical consultation |
Impact | Several papers in microgyros. New control methods for MRIG |
Start Year | 2010 |