1 st MEMS Commercial Tuning Fork Gyroscope Draper Labs M. Weinberg, J. Bernstein, S. Cho, A. T. King, A. Kourepenis, P. Ward, and J. Sohn, A micromachined.

Slides:



Advertisements
Similar presentations
4 Operation, mechanisms and applications
Advertisements

It is very difficult to measure the small change in volume of the mercury. If the mercury had the shape of a sphere, the change in diameter would be very.
Israeli Universal Spacecraft Bus Characteristics and Design Trade-Offs
Aaron Burg Azeem Meruani Michael Wickmann Robert Sandheinrich
Company Presentation.
Learning with Purpose Control Design and Implementation of a Small-Scale Autonomous Hovercraft Ryan Mackay Joshua Bevan Nicholas Lutz Mario Stamatiou University.
Calibration and Applications of a rotational sensor Chin-Jen Lin, George Liu Institute of Earth Sciences, Academia Sinica, Taiwan.
Systems and sensors Dr. Bertrand Dano ©Altapic.com, 2014.
Using inertial navigation systems (INS) to navigate
Accelerometers and Gyros Timothy Friez Class # 3 1/29/08.
“Mapping while walking”
© Copyright 2011 MicroStrain Inc. High Performance Miniature Inertial Measurement Systems MicroStrain Inc Mike Robinson
Simbeeotic: A Simulator and Testbed for Micro-Aerial Vehicle Swarm Experiments Bryan Kate, Jason Waterman, Karthik Dantu and Matt Welsh Presented By: Mostafa.
The Venus SAGE Atmospheric Structure Investigation Anthony Colaprete Dave Crisp Clayton La Baw Stephanie Morse.
Inertial Navigation Systems and GPS Juan Jacobo Van der Dys April 20 th, 2005.
M ICRO -E LECTRO M ECHANICAL S YSTEMS (MEMS). MEMS Micro Electrical Mechanical Systems Practice of making and combining miniaturized mechanical and electrical.
Ryan Roberts Gyroscopes.
Measurements using Atom Free Fall
Mining Motion Sensor Data from Smartphones for Estimating Vehicle Motion Tamer Nadeem, PhD Department of Computer Science NSF Workshop on Large-Scale Traffic.
Attitude Determination and Control
Motion Sensors Market Analysis, Market Size, Analysis 2014 To 2020 Grand View Research has announced the addition of " Global Motion Sensors Market Analysis.
Dr. Shanker Balasubramaniam
Applications: Angular Rate Sensors CSE 495/595: Intro to Micro- and Nano- Embedded Systems Prof. Darrin Hanna.
presented by: Kimberly S. Elliot Parag Gupta Kyle Reed
December, Simulation of Tightly Coupled INS/GPS Navigator Ade Mulyana, Takayuki Hoshizaki December, 2001 Purdue University.
Embedded Systems Development and Applications Terrence Mak The Chinese University of Hong Kong CENG /15.
1. The Promise of MEMS to LBS and Navigation Applications Dr. Naser El-Shiemy, CEO Trusted Positioning Inc. 2.
1 Inertial Sensors  Inertial Sensors? Inertial sensors in inertial navigation : big & expensive MEMS(Micro-Electro-Mechanical Systems) Technology  Accelerometer.
An INS/GPS Navigation System with MEMS Inertial Sensors for Small Unmanned Aerial Vehicles Masaru Naruoka The University of Tokyo 1.Introduction.
IMU 1 MicroElectroMechanical Systems (MEMS) Inertial Measurement Unit (IMU) Attitude relative to gravity vector Magnetic heading Rotational velocity Translational.
Unmanned aerial systems, what they are and what is available? Professor Sandor M Veres University of Sheffield.
Development of a Fully Autonomous Micro Aerial Vehicle for Ground Traffic Surveillance Aerospace Systems, University of Braunschweig.
Computer Vision Group Prof. Daniel Cremers Autonomous Navigation for Flying Robots Lecture 3.2: Sensors Jürgen Sturm Technische Universität München.
Autonomous Surface Navigation Platform Michael Baxter Angel Berrocal Brandon Groff.
1 SAE Aerospace Control and Guidance Systems, 2006 Lake Tahoe, NV 1-3 March 2006 Tye Brady The Inertial Stellar Compass (ISC) Tye Brady.
Accuracy Evaluation of Stereo Vision Aided Inertial Navigation for Indoor Environments D. Grießbach, D. Baumbach, A. Börner, S. Zuev German Aerospace Center.
Innovative Control Systems for MEMS Inertial Sensors Michael Kraft Reuben Wilcock Bader Almutairi Fang Chen Pejwaak Salimi.
Sérgio Ronaldo Barros dos Santos (ITA-Brazil)
Jason Choi Professor Andrei Shkel Adam Schofield, Alex Trusov, Ozan Anac.
KAITLIN PERANSKI: IE, PROJECT MANAGER JEREMY BERKE: EE, SCRIBE/LEAD SOFTWARE CHRIS CAPORALE: EE, LEAD HARDWARE SPENCER WASILEWSKI: ME, MODELING/MACHINIST.
IMPROVE THE INNOVATION Today: High Performance Inertial Measurement Systems LI.COM.
Autonomous Guidance Navigation and Control Michael Gillham University of Kent SYSIASS Meeting University of Essex
INS: Inertial Navigation Systems An overview of 4 sensors.
Outstanding Performance in Underwater Technology Tritech Positioning & RAMS™ USBL, MRU, INS & Integrity Monitoring.
INEMO™ Demonstration Kit DOF (Degrees of Freedom) platform  The STEVAL-MKI062V2 combines accelerometers, gyroscopes and magnetometers with pressure.
Applications of Virtual Reality Military –Predator Drone Miners / NASA –Distant and Dangerous Doctors –Antarctica.
Thermal Camera Systems CHILI Jalapeno Habanero. 640 x µm HgCdTe (Mercury Cadmium Telluride) long-wave thermal Less Glint from water Low Life Cycle.
Quadcopters A CEV Talk. Agenda Flight PreliminariesWhy Quadcopters The Quadcopter SystemStability: The NotionSensors and FusionControl AlgorithmsThe Way.
A Low-Cost and Fail-Safe Inertial Navigation System for Airplanes Robotics 전자공학과 깡돌가
Contents: 1. Introduction 2. Gyroscope specifications 3. Drift rate compensation 4. Orientation error correction 5. Results 6. Gyroscope and odometers.
By: Stuti Vyas( ) Drashti Sheth( ) Jay Vala( ) Internal Guide Mr. J. N. Patel.
Strapdown Inertial Navigation Systems (INS) Sensors and UAVs Avionic
MEMS GYROSCOPE By:.
EE 495 Modern Navigation Systems
Sensor Error Characteristics By: Hector Rotstein.
Sensors Fusion for Mobile Robotics localization
Trends in Automobile Innovation
Critical Design Review
MEMs Sensors Max Tesch.
Autonomous Cyber-Physical Systems: Sensing
MEMs Sensors Max Tesch.
Today’s Smart Sensors January 25, 2013 Randy Frank.
Using inertial navigation systems (INS) to navigate
Gyroscopes Eric Ruben Mechatronics Literature Survey
Inertial Measurement Units
Name Of The College & Dept
MEMS: Basic structures & Current Applications
Multi Stage Engineering
Image Acquisition and Processing of Remotely Sensed Data
Application of Inclinometer in Wind Turbine Health Monitoring.
Presentation transcript:

1 st MEMS Commercial Tuning Fork Gyroscope Draper Labs M. Weinberg, J. Bernstein, S. Cho, A. T. King, A. Kourepenis, P. Ward, and J. Sohn, A micromachined comb-drive tuning fork gyroscope for commercial applications, in Proc. Sensor Expo, Cleveland, OH, 1994, pp. 187–193. Area 1mm 2 !

A Quartz Tuning Fork Gyroscope

Economy of Scale to Lower Cost A Critical Review of MEMS Gyroscopes Technology and Commercialization Status Steven Nasiri, x108, 3150A Coronado Drive, Santa Clara, California high volume occurred once unit prices achieved $3 target prices.

Automotive: vehicle stability control, rollover detection, navigation, load leveling/suspension control, event recording, collision avoidance Consumer: computer input devices, handheld computing devices, game controllers, virtual reality gear, sports equipment, camcorders, robots Industrial: navigation of autonomous (robotic) guided vehicles, motion control of hydraulic equipment or robots, platform stabilization of heavy machinery,human transporters, yaw rate control of wind-power plants Aerospace/military: platform stabilization of avionics, stabilization of pointing systems for antennas, unmanned air vehicles, or land vehicles, inertial measurement units for inertial navigation Applications A Critical Review of MEMS Gyroscopes Technology and Commercialization Status Steven Nasiri, x108, 3150A Coronado Drive, Santa Clara, California 95054

UI Research Project- Using AUVs to Measure Magnetic Signature of Naval Vessels

IMU DAU Magnetometer

Archangel IM3 Data Resolution Body Rates 200 Hz Accelerations Hz Data Accuracy (Gyro IMU Mode) Random Walk 2.5°/hour (C1) 5.2°/hour (C2) Bias Drift 15°/hour Stability 50°/hr/year Scale Factor Accuracy 0.1% of Full Scale Scale Factor Drift 300 ppm, 1 sigma Cross Axis 0.13% maximum Data Accuracy (Accelerometer) Bias Drift 0.2 mg Scale Factor Accuracy 0.10% of Full Scale Scale Factor Drift 500 ppm, 1 sigma Cross Axis 0.13% maximum Dynamic Range - C1 ±150°/s ±10 g (Linear) - C2 ±300°/s ±10 g Bandwidth (3 db) Rates 40 Hz Maximum Accelerations 50 Hz Maximum IMU Specifications