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.
 
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