Utilising Accelerometer and Gyroscope in Smartphone to Detect Incidents on a Test Track for Cars
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Wireless Accelerometer - G-Force Max & Avg
The Leader in Low-Cost, Remote Monitoring Solutions Wireless Accelerometer - G-Force Max & Avg General Description Monnit Sensor Core Specifications The RF Wireless Accelerometer is a digital, low power, • Wireless Range: 250 - 300 ft. (non line-of-sight / low profile, capacitive sensor that is able to measure indoors through walls, ceilings & floors) * acceleration on three axes. Four different • Communication: RF 900, 920, 868 and 433 MHz accelerometer types are available from Monnit. • Power: Replaceable batteries (optimized for long battery life - Line-power (AA version) and solar Free iMonnit basic online wireless (Industrial version) options available sensor monitoring and notification • Battery Life (at 1 hour heartbeat setting): ** system to configure sensors, view data AA battery > 4-8 years and set alerts via SMS text and email. Coin Cell > 2-3 years. Industrial > 4-8 years Principle of Operation * Actual range may vary depending on environment. ** Battery life is determined by sensor reporting Accelerometer samples at 800 Hz over a 10 second frequency and other variables. period, and reports the measured MAXIMUM value for each axis in g-force and the AVERAGE measured g-force on each axis over the same period, for all three axes. (Only available in the AA version.) This sensor reports in every 10 seconds with this data. Other sampling periods can be configured, down to one second and up to 10 minutes*. The data reported is useful for tracking periodic motion. Sensor data is displayed as max and average. Example: • Max X: 0.125 Max Y: 1.012 Max Z: 0.015 • Avg X: 0.110 Avg Y: 1.005 Avg Z: 0.007 * Customer cannot configure sampling period on their own. -
Measurement of the Earth Tides with a MEMS Gravimeter
1 Measurement of the Earth tides with a MEMS gravimeter ∗ y ∗ y ∗ ∗ ∗ 2 R. P. Middlemiss, A. Samarelli, D. J. Paul, J. Hough, S. Rowan and G. D. Hammond 3 The ability to measure tiny variations in the local gravitational acceleration allows { amongst 4 other applications { the detection of hidden hydrocarbon reserves, magma build-up before volcanic 5 eruptions, and subterranean tunnels. Several technologies are available that achieve the sensi- p 1 6 tivities required for such applications (tens of µGal= Hz): free-fall gravimeters , spring-based 2; 3 4 5 7 gravimeters , superconducting gravimeters , and atom interferometers . All of these devices can 6 8 observe the Earth Tides ; the elastic deformation of the Earth's crust as a result of tidal forces. 9 This is a universally predictable gravitational signal that requires both high sensitivity and high 10 stability over timescales of several days to measure. All present gravimeters, however, have limita- 11 tions of excessive cost (> $100 k) and high mass (>8 kg). We have built a microelectromechanical p 12 system (MEMS) gravimeter with a sensitivity of 40 µGal= Hz in a package size of only a few 13 cubic centimetres. We demonstrate the remarkable stability and sensitivity of our device with a 14 measurement of the Earth tides. Such a measurement has never been undertaken with a MEMS 15 device, and proves the long term stability of our instrument compared to any other MEMS device, 16 making it the first MEMS accelerometer to transition from seismometer to gravimeter. This heralds 17 a transformative step in MEMS accelerometer technology. -
A GUIDE to USING FETS for SENSOR APPLICATIONS by Ron Quan
Three Decades of Quality Through Innovation A GUIDE TO USING FETS FOR SENSOR APPLICATIONS By Ron Quan Linear Integrated Systems • 4042 Clipper Court • Fremont, CA 94538 • Tel: 510 490-9160 • Fax: 510 353-0261 • Email: [email protected] A GUIDE TO USING FETS FOR SENSOR APPLICATIONS many discrete FETs have input capacitances of less than 5 pF. Also, there are few low noise FET input op amps Linear Systems that have equivalent input noise voltages density of less provides a variety of FETs (Field Effect Transistors) than 4 nV/ 퐻푧. However, there are a number of suitable for use in low noise amplifier applications for discrete FETs rated at ≤ 2 nV/ 퐻푧 in terms of equivalent photo diodes, accelerometers, transducers, and other Input noise voltage density. types of sensors. For those op amps that are rated as low noise, normally In particular, low noise JFETs exhibit low input gate the input stages use bipolar transistors that generate currents that are desirable when working with high much greater noise currents at the input terminals than impedance devices at the input or with high value FETs. These noise currents flowing into high impedances feedback resistors (e.g., ≥1MΩ). Operational amplifiers form added (random) noise voltages that are often (op amps) with bipolar transistor input stages have much greater than the equivalent input noise. much higher input noise currents than FETs. One advantage of using discrete FETs is that an op amp In general, many op amps have a combination of higher that is not rated as low noise in terms of input current noise and input capacitance when compared to some can be converted into an amplifier with low input discrete FETs. -
A Tuning Fork Gyroscope with a Polygon-Shaped Vibration Beam
micromachines Article A Tuning Fork Gyroscope with a Polygon-Shaped Vibration Beam Qiang Xu, Zhanqiang Hou *, Yunbin Kuang, Tongqiao Miao, Fenlan Ou, Ming Zhuo, Dingbang Xiao and Xuezhong Wu * College of Intelligence Science and Engineering, National University of Defense Technology, Changsha 410073, China; [email protected] (Q.X.); [email protected] (Y.K.); [email protected] (T.M.); [email protected] (F.O.); [email protected] (M.Z.); [email protected] (D.X.) * Correspondence: [email protected] (Z.H.); [email protected] (X.W.) Received: 22 October 2019; Accepted: 18 November 2019; Published: 25 November 2019 Abstract: In this paper, a tuning fork gyroscope with a polygon-shaped vibration beam is proposed. The vibration structure of the gyroscope consists of a polygon-shaped vibration beam, two supporting beams, and four vibration masts. The spindle azimuth of the vibration beam is critical for performance improvement. As the spindle azimuth increases, the proposed vibration structure generates more driving amplitude and reduces the initial capacitance gap, so as to improve the signal-to-noise ratio (SNR) of the gyroscope. However, after taking the driving amplitude and the driving voltage into consideration comprehensively, the optimized spindle azimuth of the vibration beam is designed in an appropriate range. Then, both wet etching and dry etching processes are applied to its manufacture. After that, the fabricated gyroscope is packaged in a vacuum ceramic tube after bonding. Combining automatic gain control and weak capacitance detection technology, the closed-loop control circuit of the drive mode is implemented, and high precision output circuit is achieved for the gyroscope. -
Evaluation of Gyroscope-Embedded Mobile Phones
Evaluation of Gyroscope-embedded Mobile Phones Christopher Barthold, Kalyan Pathapati Subbu and Ram Dantu∗ Department of Computer Science and Engineering University of North Texas, Denton, Texas 76201 Email: [email protected], [email protected], [email protected] ∗ Also currently visiting professor in Massachusetts Institute of Technology. Abstract—Many mobile phone applications such as pedometers accurately determine the phone’s orientation. Similar mobile and navigation systems rely on orientation sensors that most applications cannot be used in real-life situations without smartphones are now equipped with. Unfortunately, these sensors knowing the device’s orientation to virtually orient it. rely on measured accelerometer and magnetic field data to determine the orientation. Thus, accelerations upon the phone The two principle problems we face are, 1) the varying which arise from everyday use alter orientation information. orientation of the device when placed in user pockets, hand- Similarly, external magnetic interferences from indoor/urban bags or held in different positions, and 2) existence of user settings affect the heading calculation, resulting in inaccurate acceleration and external magnetic fields. A potential solution directional information. The inability to determine the orientation to these problems could be the use of gyroscopes, which are during everyday use inhibits many potential mobile applications development. devices that can detect orientation change. These sensors are In this work, we exploit the newly built-in gyroscope in known to be immune to external accelerations and magnetic the Nexus S smartphone to address the interference problems interferences. MEMS based gyroscopes have already found associated with the orientation sensor. We first perform drift error their way in handhelds, tablets, digital cameras to name a few. -
Basic Principles of Inertial Navigation
Basic Principles of Inertial Navigation Seminar on inertial navigation systems Tampere University of Technology 1 The five basic forms of navigation • Pilotage, which essentially relies on recognizing landmarks to know where you are. It is older than human kind. • Dead reckoning, which relies on knowing where you started from plus some form of heading information and some estimate of speed. • Celestial navigation, using time and the angles between local vertical and known celestial objects (e.g., sun, moon, or stars). • Radio navigation, which relies on radio‐frequency sources with known locations (including GNSS satellites, LORAN‐C, Omega, Tacan, US Army Position Location and Reporting System…) • Inertial navigation, which relies on knowing your initial position, velocity, and attitude and thereafter measuring your attitude rates and accelerations. The operation of inertial navigation systems (INS) depends upon Newton’s laws of classical mechanics. It is the only form of navigation that does not rely on external references. • These forms of navigation can be used in combination as well. The subject of our seminar is the fifth form of navigation – inertial navigation. 2 A few definitions • Inertia is the property of bodies to maintain constant translational and rotational velocity, unless disturbed by forces or torques, respectively (Newton’s first law of motion). • An inertial reference frame is a coordinate frame in which Newton’s laws of motion are valid. Inertial reference frames are neither rotating nor accelerating. • Inertial sensors measure rotation rate and acceleration, both of which are vector‐ valued variables. • Gyroscopes are sensors for measuring rotation: rate gyroscopes measure rotation rate, and integrating gyroscopes (also called whole‐angle gyroscopes) measure rotation angle. -
Evaluation of MEMS Accelerometer and Gyroscope for Orientation Tracking Nutrunner Functionality
EXAMENSARBETE INOM ELEKTROTEKNIK, GRUNDNIVÅ, 15 HP STOCKHOLM, SVERIGE 2017 Evaluation of MEMS accelerometer and gyroscope for orientation tracking nutrunner functionality Utvärdering av MEMS accelerometer och gyroskop för rörelseavläsning av skruvdragare ERIK GRAHN KTH SKOLAN FÖR TEKNIK OCH HÄLSA Evaluation of MEMS accelerometer and gyroscope for orientation tracking nutrunner functionality Utvärdering av MEMS accelerometer och gyroskop för rörelseavläsning av skruvdragare Erik Grahn Examensarbete inom Elektroteknik, Grundnivå, 15 hp Handledare på KTH: Torgny Forsberg Examinator: Thomas Lind TRITA-STH 2017:115 KTH Skolan för Teknik och Hälsa 141 57 Huddinge, Sverige Abstract In the production industry, quality control is of importance. Even though today's tools provide a lot of functionality and safety to help the operators in their job, the operators still is responsible for the final quality of the parts. Today the nutrunners manufactured by Atlas Copco use their driver to detect the tightening angle. There- fore the operator can influence the tightening by turning the tool clockwise or counterclockwise during a tightening and quality cannot be assured that the bolt is tightened with a certain torque angle. The function of orientation tracking was de- sired to be evaluated for the Tensor STB angle and STB pistol tools manufactured by Atlas Copco. To be able to study the orientation of a nutrunner, practical exper- iments were introduced where an IMU sensor was fixed on a battery powered nutrunner. Sensor fusion in the form of a complementary filter was evaluated. The result states that the accelerometer could not be used to estimate the angular dis- placement of tightening due to vibration and gimbal lock and therefore a sensor fusion is not possible. -
Full Auto-Calibration of a Smartphone on Board a Vehicle Using IMU and GPS Embedded Sensors
Full auto-calibration of a smartphone on board a vehicle using IMU and GPS embedded sensors Javier Almaz´an, Luis M. Bergasa, J. Javier Yebes, Rafael Barea and Roberto Arroyo Abstract| Nowadays, smartphones are widely used Smartphones provide two kinds of measurements. The in the world, and generally, they are equipped with first ones are relative to the world, such as GPS and many sensors. In this paper we study how powerful magnetometers. The second ones are relative to the the low-cost embedded IMU and GPS could become for Intelligent Vehicles. The information given by device, such as accelerometers and gyroscopes. Knowing accelerometer and gyroscope is useful if the relations the relation between the smartphone reference system between the smartphone reference system, the vehicle and the world reference system is very important in order reference system and the world reference system are to reference the second kind of measurements globally [3]. known. Commonly, the magnetometer sensor is used In other words, working with this kind of measurements to determine the orientation of the smartphone, but its main drawback is the high influence of electro- involves knowing the pose of the smartphone in the magnetic interference. In view of this, we propose a world. novel automatic method to calibrate a smartphone Intelligent Vehicles can be helped by using in-vehicle on board a vehicle using its embedded IMU and smartphones to measure some driving indicators. On the GPS, based on longitudinal vehicle acceleration. To one hand, using smartphones requires no extra hardware the best of our knowledge, this is the first attempt to estimate the yaw angle of a smartphone relative to a mounted in the vehicle, offering cheap and standard vehicle in every case, even on non-zero slope roads. -
Accelerometer and Gyroscope Design Guidelines
Application Note Accelerometer and Gyroscope Design Guidelines PURPOSE AND SCOPE This document provides high-level placement and layout guidelines for InvenSense MotionTracking™ devices. Every sensor has specific requirements in order to ensure the highest level of performance in a finished product. For a layout assessment of your design, and placement of your components, please contact InvenSense. InvenSense Inc. InvenSense reserves the right to change the detail 1745 Technology Drive, San Jose, CA 95110 U.S.A Document Number: AN-000016 specifications as may be required to permit +1(408) 988–7339 Revision: 1.0 improvements in the design of its products. www.invensense.com Release Date: 10/07/2014 TABLE OF CONTENTS PURPOSE AND SCOPE .......................................................................................................................................................................... 1 1. ACCELEROMETER AND GYROSCOPE DESIGN GUIDELINES ....................................................................................................... 3 1.1 PACKAGE STRESS .......................................................................................................................................................... 3 1.2 PANELIZED/ARRAY PCB ................................................................................................................................................. 5 1.3 THERMAL REQUIREMENTS ......................................................................................................................................... -
Accelerometers
JOHNS HOPKINS UNIVERSITY,PHYSICSAND ASTRONOMY AS.173.111 – GENERAL PHYSICS LABORATORY I Accelerometers 1L EARNING OBJECTIVES At the conclusion of this activity you should be able to: • Use your smartphone to collect acceleration data. • Use measured acceleration to estimate the distance of a free fall • Use measured acceleration to estimate kinematic quantities that describe an elevator ride. 2B ACKGROUND 2.1A CCELERATION,VELOCITY, AND POSITION We know from Classical Mechanics that we can move between position, velocity, and acceleration by repeatedly taking time derivatives of the position of an object. Similarly, starting from acceleration, we can take subsequent integrals with respect to time to obtain velocity and position respectively. Description Differential Form Integral Form Z Position ~x ~x ~vdt Æ d~x Z Velocity ~v ~v ~adt Æ dt Æ d 2~x d~v Acceleration ~a ~a Æ dt 2 Æ dt 2.2C OLLECTING DATA WITH A SMARTPHONE Most modern smart phones come packed with sensors that make them ideal to use as physics instru- ments. Many cell phones come packaged with an air pressure sensor, light meter, 3-axis accelerometers, 3-axis magnetometer, gyroscope, and of course a microphone. Many great physics measurements can be made using your smart phone. Several apps exist for collecting data from these packaged sensors. For this lab activity, we will use the PhyPhox app. You may download the app to your phone here: https://phyphox.org/ Revised: Wednesday 10th March, 2021 16:32 ©2014 J. Reid Mumford PhyPhox is also available in both the Google Play and Apple app stores. 2.3A CCELEROMETERS Your smartphone is packaged with a small integrated circuit package called a Microelectromechanical Systems (MEMS). -
Development of MEMS Capacitive Sensor Using a MOSFET Structure
Extended Summary 本文は pp.102-107 Development of MEMS Capacitive Sensor Using a MOSFET Structure Hayato Izumi Non-member (Kansai University, [email protected]) Yohei Matsumoto Non-member (Kansai University, [email protected] u.ac.jp) Seiji Aoyagi Member (Kansai University, [email protected] u.ac.jp) Yusaku Harada Non-member (Kansai University, [email protected] u.ac.jp) Shoso Shingubara Non-member (Kansai University, [email protected]) Minoru Sasaki Member (Toyota Technological Institute, [email protected]) Kazuhiro Hane Member (Tohoku University, [email protected]) Hiroshi Tokunaga Non-member (M. T. C. Corp., [email protected]) Keywords : MOSFET, capacitive sensor, accelerometer, circuit for temperature compensation The concept of a capacitive MOSFET sensor for detecting voltage change, is proposed (Fig. 4). This circuitry is effective for vertical force applied to its floating gate was already reported by compensating ambient temperature, since two MOSFETs are the authors (Fig. 1). This sensor detects the displacement of the simultaneously suffer almost the same temperature change. The movable gate electrode from changes in drain current, and this performance of this circuitry is confirmed by SPICE simulation. current can be amplified electrically by adding voltage to the gate, The operating point, i.e., the output voltage, is stable irrespective i.e., the MOSFET itself serves as a mechanical sensor structure. of the ambient temperature change (Fig. 5(a)). The output voltage Following this, in the present paper, a practical test device is has comparatively good linearity to the gap length, which would fabricated. -
Gravitation and Geodesy with Inertial Sensors, from Ground to Space
Testing in Aerospace Research P. Touboul (ONERA) Gravitation and Geodesy G. Métris (Geoazur – CNRS/UMR) with Inertial Sensors, H. Sélig from Ground to Space (ZARM Space Science Department University of Bremen) ince the years 2000, three space missions, CHAMP, GRACE, and GOCE, have led S us to consider the Earth's gravitational field and its measurement in a new light, O. Le Traon, A. Bresson, using dedicated sensors and adequate data processing, revealing the changes in the N. Zahzam, B. Christophe, M. Rodrigues Earth's field as the true signal rather than the disturbing terms in addition to the geo- (ONERA) static reference field. Besides the possibilities offered by new technologies for the development of inertial sensors, a space environment of course involves special con- E-mail: [email protected] straints, but also allows the possibility of a specific optimization of the concepts and techniques well suited for microgravity conditions. We will analyze and compare with DOI: 10.12762/2016.AL12-11 others the interest in the electrostatic configuration of the instruments used in the main payload of these missions, and we will consider the recent MICROSCOPE mission, which takes advantage of the same mission configuration as a gradiometry mission to test the universality of free fall whatever the mass composition. A few days after launching the satellite in April 2016, we will show how we intend to validate the future result, the existence or not of a violation signal of the equivalence principle, taking into account the laboratory tests, where available, and the in-flight demonstrated perfor- mance during the calibration phases and the scientific measurements.