Gyroscopes
Measure or maintain a single distance in relation to an object, regardless of shift in angle.
See Also: IMU, Accelerometers, Flywheel
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Gyroscopes
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A device consisting of a wheel or disk mounted so that it can spin rapidly about an axis that is itself free to alter in direction. The orientation of the axis is not affected by tilting of the mounting; so gyroscopes can be used to provide stability or maintain a reference direction in navigation systems, automatic pilots, and stabilizers.
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Gyroscopes
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Analog Devices MEMS gyroscopes and iSensor® MEMS gyroscope subsystems reliably sense and measure the angular rate of an object under complex and severe operating conditions. Our MEMS gyroscope portfolio includes analog and digital output, high vibration and shock immunity, and temperature sensitivity control to 25 ppm/°C. Measure an object’s rotation in °/sec over a wide dynamic range and bandwidth while leveraging our expertise to jumpstart your next design.
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Autopilot Attitude Gyroscopes
5000E/L-series
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The 5000E air-driven attitude gyro is another variation of our standard 5000B model. It includes inductive pickoffs that generate the signals necessaryto drive an autopilot. The intuitive display has a moving horizon mask that indicates the position of the aircraft’s wings in relation to the natural horizon. This attitude information is passed along to the autopilot system.
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Heading Reference Directional Gyroscopes
4000HR-series
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The 4000HR air-driven directional gyro offers some of the best features of our other popular models. It inherited all of the functionality and reliability of the industry standard 4000B upon which it’s based, and it picked up a heading reference bug from the 4000C autopilot model.
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XYZ Bootstrap Directional Gyroscopes
4000H-series
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Sigma Tek's Directional Gyro with heading synchro output provides a cost effective link to "bootstrap" other instruments requiring heading information for: display orientation to aircraft heading, heading stabilization functions, and other navigational calculations and/or solutions. Specific applications include: Argus Moving Map Display®, L-3 Avionics Stormscope®, and Insight Strike Finder®.
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Two And Three Axis Gyroscopes
TAG
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The Inertial Labs Axis Gyroscopes are developed for Electro-Optical Systems, Gimbals, Line-of-Sight, and Pan and Tilt Platforms for inertial stabilization and pointing applications. These devices utilize advanced, tactical-grade MEMS sensitivity whose size, power consumption, reliability, and performance are ideal for accomplishing complex tasks requiring accurately stabilizing assorted platforms.
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Cageable Attitude Gyroscopes
5000M-series
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The 5000M is an air-driven gyro that has a pictorial horizon mask and fixed airplane. The mask moves to indicate climb, dive, and bank. Bank and pitch attitudes are displayed so that the pilot’s sensing of the gyro indication is the same as the interpretation of the relation between the wings of the aircraft and the natural horizon during visual flight.
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Standard Directional Gyroscopes
4000B-series
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The 4000B is our standard air-driven directional gyro. As the aircraft turns left or right, gears on the sensing unit and dial shaft translate this rotation into rotation of the instrument’s vertical dial. Left turns produce clockwise dial rotation and right turns produce counter-clockwise rotation. The gyro is controlled by a heading selector knob located on the lower left of the instrument. Pressing and turning the knob first disengages the dial shaft and then resets the dial to a new heading, which results in a new course indication. Releasing the selector knob re-engages the dial shaft. The on-course position of the pointer is always at the top of the azimuth circle (0° on the dial with the aircraft headed north).
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MEMS Gyroscopes
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Safran designs and manufactures high-precision tactical grade MEMSMicroElectroMechanical System. See also gyro sensors for demanding applications. We serve a global customer base in the Defense, Industrial, Aerospace and Commercial markets with ITAR-free solutions utilized in a wide range of applications. Our miniature MEMS gyro modules offer our customers compact and cost effective solutions while maintaining high performance and accuracy requirements.
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ARINC-style Attitude Gyroscopes
1U367-series
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The 1U367 has a pictorial horizon mask and a fixed airplane. The mask moves to indicate climb, dive, and bank. Bank and pitch attitudes are diaplayed so that the pilot's sensing of the gyro's horizon indication is the same as the interpretation of the relationship between the wings of the aircraft and the natural horizon during visual flight.
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Standard Attitude Gyroscopes
5000B-series
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The 5000B is an air-driven gyro that has a pictorial horizon mask and fixed airplane. The mask moves to indicate climb, dive, and bank. Bank and pitch attitudes are displayed so that the pilot’s sensing of the gyro indication is the same as the interpretation of the relation between the wings of the aircraft and the natural horizon during visual flight.
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Rate & Inertia Sensors
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TE Connectivity (TE) provides electronic test and measurement systems, such as inertial sensors, rate sensors, and rate gyroscopes for demanding industrial, military, aerospace, automotive crash testing, robotics, biomechanics, and more.
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MEMS Handler
4664-IH
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The ULTRA P is a high performance production handler that provides thermal conditioning, full 6 DOF mechanical stimulus and an electrical ATE signal path for testing Micro-Electro-Mechanical Systems (MEMS) Accelerometers and Gyroscopes.
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SLD Light Source
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The SLD light source is a light source to emit low-coherence light with a broad spectrum like LED and high brightness like LD. Light emitted from a narrow active layer like LD effectively couple to the fiber. SLD light source can be used for optical measurements and sensors, including fiber optic gyroscopes and OCT. FiberLabs provides fiber-output SLD light sources in different wavelength bands from visible to near-infrared light. Our lineup includes bench-top types convenient for experiments and easy-to-integrate module types.
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Test Sockets
MEMS Device
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Patented MEMS Sockets from Ardent Concepts use a unique scrubbing action contact set which is ideal for today’s sensitive MEMS devices, including accelerometers, gyroscopes, MEMS microphones and other specialized devices used in mobile electronics applications
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Inertial Measurement Units (IMU)
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Inertial Measurement Unit (IMU) sensors integrate multiaxis combinations of precision gyroscopes, accelerometers, magnetometers, and pressure sensors, intelligently fused to provide reliable position and motion discernment for stabilization and navigation applications. Precision MEMs IMUs deliver the required accuracy levels even in complex operating environments and under dynamic or extreme motion dynamics. ADI iSensor® IMU technology has been uniquely developed to reliably provide the high performance necessary to enable emerging applications in autonomous machinery and instruments, across multiple markets.
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Programmable Sensor Module With CAN Connection
PCAN GPS
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The PCAN-GPS is a freely programmable sensor module for position and attitude determination. It has a satellite receiver, a magnetic field sensor, an accelerometer and a gyroscope. The recorded data can be transmitted on a CAN bus and logged on the internal memory card. The data is processed by a microcontroller from the NXP LPC4000 series.
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Accelerometor, Gyro, Magnetometer Breakout Board
SEN-38001
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The LSM9DS1 is a highly configurable, flexible and precise motion sensing solution from ST Microelectronics - the latest in a wide-ranging inertial product line. It integrates a 3-axis accelerometer, 3-axis gyroscope and 3-axis magnetometer into a single IC , giving you a full nine degrees of freedom (9-DOF) in a tiny 3mm x 3.5mm package. Even with support components, square mounting pattern and connection breakouts for both SPI and I2C, this board is barely the size of a quarter.
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Bench-Top Type ASE Light Source
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ASE(Amplified Spontaneous Emission) light sources are low-coherent light sources ,which combines the both features of high intensity like laser and broad spectrum like LED. Output stability is greater than those of LD and LED, and therefore they are suitable for high accuracy measurement applications. With the use of rare-earth-doped fluoride fibers, the plentiful lineup of FiberLabs light sources includes the 540 nm-, 850 nm-, 1300 nm-, 1480 nm- and SCL-bands that other companies do not provide.They are the best light sources for FBG sensors, OCT, fiber optic gyroscopes, gas sensors, and fluorescence excitation, as well as for measurement of optical components. The bench-top type is easy to use as a stand-alone light source and the modular type is convenient for integration into equipments.
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MEMS Module
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The design and modeling of microelectromechanical systems (MEMS) is a unique engineering discipline. At small length scales, the design of resonators, gyroscopes, accelerometers, and actuators must consider the effects of several physical phenomena in their operation. Consequently, COMSOL Multiphysics is ideally suited for MEMS applications.
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SparkFun Triple Axis Accelerometer And Gyro Breakout
MPU-6050
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The MPU-6050 is a serious little piece of motion processing tech! By combining a MEMS 3-axis gyroscope and a 3-axis accelerometer on the same silicon die together with an onboard Digital Motion Processor™ (DMP™) capable of processing complex 9-axis MotionFusion algorithms, the MPU-6050 does away with the cross-axis alignment problems that can creep up on discrete parts.
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Rugged Package
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Inclinometers, Accelerometers, Gyroscopes, IMU, and AHRS Ruggedized Systems
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Optical Modules And Components
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Luna offers a complete line of high performance active and passive fiber optic modules and components for a wide range of fiber optic systems, including interferometric systems for fiber optics sensing, fiber optic gyroscope (FOG) and optical coherence tomography (OCT).
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Autopilot Directional Gyroscopes
4000C/D-series
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The 4000C/D is an air-driven directional gyro with A.C. autopilot pickoffs. Left turns produce clockwise dial rotation and right turns produce counter-clockwise rotation. Two knobs control the gyro. The left knob is used to cage the unit, and the right knob is used to select the instrument’s heading. To change course, the right selector knob is pressed and turned to disengage the dial shaft and set the pointer to a new heading. Releasing the selector knob re-engages the pointer with the dial shaft. As the aircraft turns onto a new course, the pointer returns to its original position. The on-course position of the pointer is always at the top of the azimuth circle (0° on the dial with the aircraft headed north).
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Inertia lnavigation for Civil Engineering
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Exail's Attitude and Heading Reference Systems (AHRS) and Inertial Navigation Systems (INS), incorporate Fiber-Optic Gyroscopes for reliable performance in civil engineering. Suited for tunneling, mining, construction, railway, and mobile mapping, these systems excel in challenging environments like GNSS-denied areas, ensuring undisturbed navigation, accurate georeferencing, and precise pointing amid obstacles such as buildings, trees, tunnels, and mines.
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Shield
Arduino MKR IMU Shield
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The MKR IMU Shield is based on the BNO055 absolute orientation sensor from Bosch Sensortec GmbH which integrates a triaxial 14-bit accelerometer, a triaxial 16-bit gyroscope with a range of ±2000 degrees per second and a triaxial geomagnetic sensor with a 32-bit microcontroller running the BSX3.0 FusionLib software. The sensor features three-dimensional acceleration, yaw rate and magnetic field strength data each in 3 perpendicular axes.
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Motion Simulator For Test Systems
Metis
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METIS is a motion simulator for sensor and end system level testing. Configurable design allows you to create system you need! - 1-axis rate table for gyro testing - 2-axis unit for 6DOF accelerometer and gyroscope testing - 3-axis Gimbal system for simultaneus Yaw, Pitch and Roll stimulus.
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Inertial Measurement Units
IMU
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The Inertial Labs Inertial Measurement Units (IMU) contain three highly accurate advanced MEMS gyroscopes and three high-performance accelerometers. The IMU-P and Kernel are calibrated within their operating temperature range to achieve maximum end-user usability. This also ensures tactical grade performance regardless of the environment in which it is used.
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Inertial Navigation Systems
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An inertial navigation system (INSAn INS or Inertial Navigation System - sometimes used synonomously with IMU is a device used to measure a vehicle's speed, position, velocity, heading and orientation by using an accelerometer and a gyroscope.) is a high-tech navigator using motion and rotation sensors alongside a computer to figure out where something is, how it’s moving, and how fast. By using dead reckoning, the INS method for knowing positioning, it continuously calculates an object’s position and orientation based on its initial location. This allows users in airplanes, submarines, or even spacecrafts to guide and keep track of their location without signals such as GPSGlobal Positioning System is a navigation satellite system. See also.
