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Supplier: Mid-Continent Instruments and Avionics
Description: Rate Gyro Transmitter Manufactured by Mid-Continent Instruments and Avionics
- Rate vs. Rate-integrating Gyro: Rate Gyro
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Supplier: Mid-Continent Instruments and Avionics
Description: Rate Gyro Obsolete Manufactured by Century Flight
- Rate vs. Rate-integrating Gyro: Rate Gyro
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Supplier: Mid-Continent Instruments and Avionics
Description: Rate Gyro 28V Manufactured by ARC
- Rate vs. Rate-integrating Gyro: Rate Gyro
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Supplier: Mid-Continent Instruments and Avionics
Description: Rate Gyro 14V Manufactured by ARC
- Rate vs. Rate-integrating Gyro: Rate Gyro
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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 (FOGs
- Angular / Rotary Axes: Uniaxial
- Angular Rate Range: 300 deg/sec
- Bandwidth: 200 Hz
- Bias Stability: 0.4000 deg/hr
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Supplier: Accuris
Description: RATE INTEGRATING GYRO
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Supplier: SAE International
Description: Technical Standard
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Supplier: Gladiator Technologies, Inc.
Description: temperature. The unit is highly durable and can withstand environmental vibration and shock typically associated with commercial stabilization and aerospace requirements. The MEMS G300D gyro is offered at 100°/s or 300°/s rate range. The unit is temperature compensated for bias and
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Supplier: SAE International
Description: This specification covers that gyroscopic instrument normally defined as a "subminiature rate gyro." The rate gyro, when subjected to an angular rate about its input axis, provides an AC output voltage proportional to the angular rate. The subminiature size
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Supplier: Gladiator Technologies, Inc.
Description: temperature. Designed for commercial stabilization and aircraft applications, the gyro has a bipolar "VSG compatible" signal outputting balanced 0V ± 5V. The unit is highly durable and can withstand environmental vibration and shock typically associated with commercial aerospace requirements.
- Angular / Rotary Axes: Uniaxial
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Supplier: PCB Piezotronics, Inc.
Description: 8,000 deg/sec, 15 ft cable
- Angular Rate Range: 8000 deg/sec
- Rate vs. Rate-integrating Gyro: Rate Gyro
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Supplier: Accuris
Description: Rate Gyro Assembly Configuration
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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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Description: This specification defines the requirements for a single-degree-of-fre edom 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
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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 / Rotary Axes: Triaxial
- Angular Rate Range: 125 deg/sec
- Bandwidth: 100 Hz
- Electrical Output: Pulse / Frequency
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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
- Angular / Rotary Axes: Uniaxial
- Angular Rate Range: 0.0 to 3200 deg/sec
- Bandwidth: 256 Hz
- Bias Stability: 2 to 12 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 / Rotary Axes: Uniaxial
- Angular Rate Range: 1500 deg/sec
- Bandwidth: 1000 Hz
- Electrical Output: Analog Voltage
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Supplier: OFIL Systems
Description: . DayCor® ROM HD is a 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
- Physical Features: Outdoor Rated
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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 on
- Accuracy: 0.5000 to 2 degrees
- Form Factor: Module / Standalone
- Number of Axes: 3
- Operating Temperature: -40 to 158 F
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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: LORD MicroStrain Sensing Systems
Description: Overview The 3DM-GX3® -15-OEM 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 on-board processor running a sophisticated sensor fusion
- Angular / Rotary Axes: Triaxial
- Angular Rate Range: 50 to 1200 deg/sec
- Bandwidth: 440 Hz
- Bias Stability: 18 deg/hr
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Supplier: TE Connectivity
Description: FS Range (±) DEG/SEC : 1500 Packaging Features Rate & Inertial Sensor Package : Anodized Aluminium Product Type Features Rate & Inertial Sensor Type : Rate
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Supplier: Richardson RFPD
Description: ±50°/s Yaw Rate Gyro
- Category: Development Board
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Supplier: Kionix, Inc.
Description: The KGY13 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 / Rotary Axes: Triaxial
- Angular Rate Range: 256 to 2048 deg/sec
- Angular Transverse Sensitivity: 1 ±% Full Scale
- Bandwidth: 80 Hz
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Description: MODULE GYRO RATE SENSOR 24LD
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Supplier: Aerotech, Inc.
Description: Design Features Continuous 360 degree rotation of azimuth and elevation including built-in slip ring High accuracy angular position and rate capability Direct-drive brushless servomotors result in zero backlash Cog-free design for outstanding velocity
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Supplier: Gladiator Technologies, Inc.
Description: up to 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
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Supplier: OFIL Systems
Description: evaluate dispersant operations. Recorded data is valuable for long term analysis and formulate guidelines. ORSOLAR is light in weight, simple to install and configured for gyro stabilized gimbaled payloads of sizes and mounts that match most
- Application / Industry: Industrial
- Camera Function: Still, Video
- Features: High Definition, Dome, Outdoor Rated
- Imaging Technology / Camera Type: Digital, UV
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Supplier: Memsense, LLC
Description: to be 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
- Acceleration: -8 to 8 g
- Minimum Accuracy: 0.3000 +/-% FS
- Number of Axes: Triaxial
- Operating Temperature: -40 to 85 F
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Supplier: SBG Systems SAS
Description: performance for a cost-effective solution: 0.05° Attitude over 360° AHRS, Vertical Gyro, MRU, IMU 200 Hz Output Rate 5 cm Real-time Auto Adjusting Heave 2.5 cm Delayed Heave Maintenance Free
- Angular / Rotary Axes: Triaxial
- Angular Rate Range: 400 deg/sec
- Bandwidth: 100 Hz
- Bias Stability: 3 deg/hr
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Supplier: Airmar Technology Corporation
Description: . These sensors gives heading, 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
- Device Classification: Sensor System
- Interface Options: Serial Interface
- Measures Barometric Pressure: Yes
- Measures Temperature: Yes
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Supplier: RS Components, Ltd.
Description: Analog Devices range of single, dual and 3 axis gyroscopes measure the angular rate of an object. ADIs range of MEMS and iSensor MEMS Gyros measure the rotation of an object in degrees per second over a wide dynamic range and bandwidth. Some products also offer on chip signal signal
- Package Type / Mounting: Other
- Sensor Type: Acceleration Sensor
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Supplier: QUALCOMM, Incorporated
Description: sensor Temperature sensor Pressure sensor Magnetometer sensor Humidity sensor Gyro/angular rate sensor
- Technology: Bluetooth
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Supplier: Northrop Grumman Corporation
Description: targeting gyro-compassing applications in a small package with high shock and rate capabilities. The G-2000 DTG was designed for strapdown use in tactical situations. Its accuracy is enhanced by a servo-electronics card that is specifically tailored to maximize the performance of this
- Angular / Rotary Axes: Biaxial, Triaxial
- Angular Rate Range: 60 to 285 deg/sec
- Operating Temperature: -40 to 185 F
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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
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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
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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.