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Supplier: Mid-Continent Instruments and Avionics
Description: Rate Gyro Transmitter Manufactured by Mid-Continent Instruments and Avionics
- Gyro Type: Rate Gyro
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Supplier: Accuris
Description: Rate Gyro Assembly Configuration
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Supplier: Accuris
Description: RATE INTEGRATING GYRO
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Supplier: Mid-Continent Instruments and Avionics
Description: Turn and Bank Indicator Repair only â€" 90-day warranty Manufactured by Instruments Inc
- Gyro Type: Rate Gyro
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Supplier: Mid-Continent Instruments and Avionics
Description: Turn Coordinator 14V, Autopilot Manufactured by S-Tec for AIM
- Gyro Type: Rate Gyro
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Supplier: SAE International
Description: Technical Standard
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Supplier: Mid-Continent Instruments and Avionics
Description: Turn Coordinator 28V, Lighted, Twinstar AS350 / MBB B-105 Manufactured by AIM for Aerospatiale
- Gyro Type: Rate Gyro
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Supplier: Accuris
Description: Single-Degree-of-Freedom Spring-Restrained Rate Gyros
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Description: Recommended rate gyro test procedures derived from those currently in use, including test conditions to be considered, are compiled. In some cases alternate methods for measuring a performance characteristic have been included. This standard is intended to be a guide in the preparation
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Description: This specification defines the requirements for a single-degree-of-freedom spring-restrained rate gyro for [aircraft, missile, spacecraft,______] applications. The rate gyro shall be capable of providing [(dc, ac) voltage outputs proportional to angular rate inputs
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Description: This specification defines the requirements for a single-degree-of-freedom rate-integrating gyro to be used as a sensor in systems such as an attitude control system, a gimbal platform, an angular displacement measuring system, or an angular rate measuring system. The external
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Supplier: Gladiator Technologies, Inc.
Description: The G300D Gyro represents Gladiator's breakthrough gyro technology enabling an ultra low noise tri-axis MEMS gyro and bandwidth of 250Hz that has performance commensurate with much more expensive small Dynamically Tuned Gyros. It also features industry leading bias in-run
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Supplier: Gladiator Technologies, Inc.
Description: G150Z Gyro represents Gladiator's breakthrough gyro technology enabling an ultra low noise MEMS gyro and bandwidth of 200Hz that has performance commensurate with much more expensive small RLG's and small open loop FOG's. The G150Z also features industry leading bias in-run and
- Angular / Rotary Axes: Uniaxial
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Supplier: Jewell Instruments, LLC
Description: precision 3-axis solid-state magnetometer. Two angular rate gyros independently stabilize pitch and roll. They augment a dual-axis, electrolytic tilt sensor that provides precise tilt measurements in static environments. Two sets of independent filters, one set for pitch and one for
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Supplier: Tronics Microsystems
Description: GYPRO4300 redefines performance in dynamic applications, delivering exceptional stability and repeatability for precise positioning and motion control, even under severe vibration conditions. This closed-loop MEMS gyro offers a digital and low-SWaP alternative to Fiber-Optic Gyroscopes
- Angular Rate Range: 300 deg/sec
- Linearity: 60 ±% Full Scale
- Bandwidth: 200 Hz
- Bias Stability: 0.4 deg/hr
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Description: The DTS Angular Rate Sensor (gyro) was introduced in late 2006 and has quickly become the industry favorite. Developed with design comment from USCAR (GM, Chrysler, Ford), Toyota, Northrup Grumman, US Airforce and other DTS clients, the DTS ARS meets and exceeds testing requirements
- Angular Rate Range: 300 deg/sec
- Bandwidth: 100 Hz
- Maximum Dimension: 0.58 inch
- Weight: 0.00661375661375661 lbs
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Supplier: Shenzhen Rion Technology Co., Ltd
Description: TL735G is a high-precision three-axis attitude meter developed by RION Technology based on the company's latest MEMS inertial measurement platform. It outputs the horizontal azimuth angle and angular rate of the object in real time by performing dynamic attitude algorithm on the angular
- Angular Rate Range: 124.9999999999998 deg/sec
- Bandwidth: 100 Hz
- Weight: 0.264550264550265 lbs
- Output Options: Pulse / Frequency
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Supplier: PCB Piezotronics, Inc.
Description: RATE SENSOR
- Output Options: Analog Voltage
- Gyro Type: Rate Gyro
- Angular / Rotary Axes: Uniaxial
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Supplier: Shenzhen Rion Technology Co., Ltd
Description: ? Real-time angular rate output? Horizontal azimuth and attitude angle output? Long life and strong stability? Forward axis acceleration
- Angular / Rotary Axes: Biaxial
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Supplier: Shenzhen Rion Technology Co., Ltd
Description: rate of the inertia unit, by integrating the angular velocity of the object, and then with the attitude angle of the multi model data fusion, can real-time update of the horizontal azimuth output. This product is specially used for robot car, AVG vehicle azimuth orientation, attitude control
- Angular Rate Range: 300 deg/sec
- Weight: 1.25661375661376 lbs
- Operating Temperature: -40 to 85 F
- Output Options: Pulse / Frequency
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Supplier: OFIL Systems
Description: powerful high-speed inspection solution for aircrafts, equipped with combinations of outstandingly highly sensitive, high definition (HD) sensors in a gyro stabilized payload platform. ROM meets the need for stability, accuracy, functionality, convenience and qualitative data collection. The
- Application / Industry: Industrial
- Features: Outdoor Rated
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Supplier: Newark, An Avnet Company
Description: SENSOR BRD, SCC2230-E02 ACCELERO/GYRO; Accessory Type:Sensor Board; For Use With:Murata MEMS Evaluation Boards; SVHC:No SVHC (07-Jul-2017); Features:Gyroscope & 3-axis Accelerometer, SPI, +/-125Deg/s Z-axis Angular Rate, +/-2g RoHS Compliant: Yes
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Supplier: TE Connectivity
Description: Dimensions Dimensions MM : 24 x 24 x 27.30 Electrical Characteristics Excitation Voltage (VDC) : 10 - 36 Other Accuracy : ±0.01% Non-Linearity FS Range (±) DEG/SEC : 450 Packaging Features Rate & Inertial Sensor Package : Anodized Aluminium Product Type Features Rate & Inertial Sensor
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Supplier: LORD MicroStrain Sensing Systems
Description: Miniature Inertial Measurement Unit And Vertical Gyro Overview The 3DM-GX3® -15 is a high-performance, miniature Inertial Measurement Unit and Vertical Gyro, utilizing MEMS sensor technology. It combines a triaxial accelerometer, triaxial gyro, temperature sensors, and an
- Tilt Angle: 360 degrees
- Number of Axes: 3
- Accuracy: 0.5 to 2 degrees
- Supply Voltage: 3.2 to 16 volts
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Supplier: Imego
Description: IBG21 is a small, rugged and shock-tolerant MEMS-based gyro system. The dual-side mounting capability allows measurement of all three rotation axes on a single mounting plane. IBG21 is based on the GyroSense concept and consists of a sensor chip, a mixed-signal ASIC and a D-ASIC assembled in
- Angular Rate Range: 0 to 3,199.999999999998 deg/sec
- Linearity: 0.025 ±% Full Scale
- Bandwidth: 256 Hz
- Bias Stability: 2 to 12.000000000000009 deg/hr
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Supplier: Aerotech, Inc.
Description: diameter Low maintenance and high reliability provide the lowest cost of ownership Aerotech's AMG position and rate gimbal mounts provide ultra-precise angular position, rate and acceleration for development and production testing of a wide range of systems. The AMG series is ideal for
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Supplier: Richardson RFPD
Description: ±50°/s Yaw Rate Gyro
- Category: Development Board
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Supplier: Aerotech, Inc.
Description: Design Features Smaller than traditional three-axis simulators to accommodate today's miniature MEMS gyros in a much smaller footprint Modular design based on the ARMS rate tables Continuous or limited travel options Pedestal options High torque three-axis systems for testing INU and
- Type: Three-axis
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Supplier: Kionix, Inc.
Description: The KGY12 series is designed to strike a balance between current consumption and noise performance with excellent bias stability over temperature. These sensors can accept supply voltages between 2.6V and 3.3V, and digital communication voltages between 1.8 and 3.3V. Sensor bandwidth is
- Angular Rate Range: 256.0000000000002 to 2,047.999999999998 deg/sec
- Bandwidth: 80 Hz
- Angular Transverse Sensitivity: 1 ±% Full Scale
- Maximum Dimension: 0.1968505 inch
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Supplier: Hottinger Bruel and Kjaer UK Ltd.
Description: The MV7-AR gyro-stabilised inclinometer delivers precision measurements of dynamic inclination, acceleration, and angular rate in challenging environments such as those encountered by heavy-duty construction, off-highway, agriculture, and trucking vehicles.
- Supply Voltage: 4.5 to 36 volts
- Operating Temperature: 185 F
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Supplier: SAE International
Description: gyros are not required. Angular rate measurements are fused with camera star measurements at raw data level. By the data processing the gyro attitude with respect to the "master camera" - denoted as "gyro on board attitude" - is estimated. The main novelty content and
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Supplier: Gladiator Technologies, Inc.
Description: 5000Hz data rate of delta velocity and delta theta. This Inertial Measurement Unit (IMU) features a small and light weight option at just 18 grams offering application versatility for users that have space constraints while still demanding outstanding performance enabled by its low noise
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Supplier: Memsense, LLC
Description: tuned to your application with configurable bandwidth, sample rate, gyro ranges, 1 PPS input and other measurement parameters. Streamline your global operation and improve performance with the MS-IMU3020 IMU that requires no export license. The inertial measurement unit provides all
- TJ: -40 to 85 C
- Features: Other
- Technology: RS422, USB
- Device Type: Transmitter
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Supplier: Airmar Technology Corporation
Description: position, speed-over-ground, and course-over-ground functionality that is required for theoretical wind-data processing and mobile applications. A 3D compass with dynamic stabilization provided by the three-axis rate gyro enhances the rate-of-turn data. Features Ultrasonic
- Operating Temperature: -13 to 131 F
- Mounting Type: Base Mounted
- Weather Component Sensed: Measures Barometric Pressure, Measures Temperature, Senses Wind Direction, Senses Wind Speed
- Output Options: Pulse Signal
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Featured Products Top
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ensure precise motion control of ships and vessels. Our high-performance digital MEMS inertial sensors offer high accuracy acceleration and angular rate measurement for integration into MRU (Motion Reference Units) used by marine applications such as ship dynamic positioning and platform (read more)
Browse Accelerometers Datasheets for Tronics Microsystems -
GYPRO®4300 is a high stability MEMS gyro tailored to GNSS-assisted inertial navigation and positioning of ground vehicles and trains, MRU (Motion Control Unit) for ship motion control and positioning, as well as AHRS for small aircrafts, helicopters, and drones, but (read more)
Browse Gyroscopes Datasheets for Tronics Microsystems -
Build compact and high-performance inertial systems with GYPRO4300, a tactical grade ± 300 °/s MEMS rate gyro able to demonstrate high stability and low drift for precise attitude determination, positioning and navigation in harsh (read more)
Browse Gyroscopes Datasheets for Tronics Microsystems -
temperature range. It is ideally complemented by GYPRO®4300, high stability 300 °/s rate gyro that exhibits an ARW of 0.07 °/√h and a bias instability of 0.4 °/h. Their fully digital (read more)
Browse Datasheets for Tronics Microsystems -
tactical-grade quartz accelerometers. AXO300 accelerometers are ideally complemented by high performance Tronics GYPRO® digital rate gyros that share the same SMD J-lead ceramic package (12 x 12 x 5 mm) and same digital interface to enable low (read more)
Browse Accelerometers Datasheets for Tronics Microsystems -
Tronics is the only provider of both closed-loop MEMS Accelerometers and Gyros, taking MEMS inertial sensors to an unrivalled level of performance. Closed-loop electronics, also called force-feedback, brings several key advantages to inertial sensors, including superior (read more)
Browse Datasheets for Tronics Microsystems
Conduct Research Top
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The Rate Integrating Gyroscope (RIG), Part 1
The gyroscope is an instrument where the input is a rate of turn (angular rate). Any gyroscope is a torque-in, torque-out device. Therefore, the output of the gyro is a change in the gimbal angle (the gimbal turns) in response to the rate of turn input, due to gyroscopic precession. The input
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Basic Output Generator Excitation and Demodulation Requirements for USD Gyroscopes
This applications note discusses the input signal excitation and output signal conditioning (demodulation) requirements of the transformer type output generator, or pickoff used on the US Dynamics Miniature Rate Integrating Gyroscopes (RIG) and Rate Gyroscopes. In addition, basic transformer type
More Information Top
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http://dspace.mit.edu/bitstream/handle/1721.1/46437/31001000-MIT.pdf?sequence=2
Rate gyro package .
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http://dspace.mit.edu/bitstream/handle/1721.1/37077/83280846-MIT.pdf?sequence=2
In this thesis, an inertial measurement unit (IMU) consisting of 3 accelerometers and 3 rate gyros is created using off-the-shelf sensors from STMicro and Analog Devices.
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http://etd.auburn.edu/bitstream/handle/10415/1908/AndersonETD2.pdf?sequence=1
packages: rate gyros only, rate gyros and an ideal magnetometer, rate gyros and a magnetometer, .
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Automatic Control of Atmospheric and Space Flight Vehicles
bank angle, , by a rate-integrating gyro, yaw rate, R, by a rate gyro (Chap. 2), and the control angles, ıE; ˇT; ıA; ıR picked-up by optical angle encoders.
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Introduction to Avionics Systems
255 5.2.2 Micro Electro-Mechanical Systems (MEMS) Technology Rate Gyros . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
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Avionics Navigation Systems 2nd Edition Complete Document
In the simplest, the gyro is mounted on a rigid table and connected as a single-axis or two-axis rate gyro , with its pickoff(s) caged to its torquer(s).
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http://etd.auburn.edu/bitstream/handle/10415/329/FLENNIKEN_WARREN_52.pdf?sequence=1
16 2.6 Rate Gyro Model Validation……………………………………..……...
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http://calhoun.nps.edu/public/bitstream/handle/10945/6229/01Dec_Chernesky.pdf?sequence=1
The platform hosts several satellite subsystems, including rate gyros , reaction wheels, thrusters, sun sensors, and an onboard control computer.
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Design of multi-sensor attitude determination systems
The systems discussed fuse information from a triad of solid state rate gyros with an aiding system mechanized using GPS or magnetometers and accelerometers.
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