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Description: This specification defines the requirements for a two-degree-of-freedo m dynamically tuned gyro to be used as a sensor in a strapdown, gimballed inertial navigation system (attitude reference units) for use in an aircraft, a missile, a spacecraft or similar applications. The
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Supplier: Gladiator Technologies, Inc.
Description: The G400D Biax Gyro represents Gladiator's breakthrough gyro technology enabling an ultra low noise biaxial digital MEMS gyro and bandwidth of 250Hz that has performance commensurate with much more expensive small Dynamically Tuned Gyros. It is designed for
- Angular / Rotary Axes: Biaxial
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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
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Supplier: Tronics Microsystems
Description: High bias stability for precision navigation and positioning in dynamic applications GYPRO®4300 is a high-performance, closed-loop digital MEMS gyroscope with ± 300 °/s input range that offers a cost-effective alternative to entry-level Fiber Optic Gyroscopes (FOG) and Dynamically
- Angular / Rotary Axes: Uniaxial
- Angular Rate Range: 300 deg/sec
- Bandwidth: 200 Hz
- Linearity: 100 ±% Full Scale
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Supplier: S&P Global Engineering Solutions
Description: SPECIFICATION FORMAT GUIDE AND TEST PROCEDURE FOR TWO-DEGREE-OF- FREEDOM DYNAMICALLY TUNED GYROS
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Supplier: Northrop Grumman Corporation
Description: The Northrop Grumman G-2000 two-axis gyroscope offers superior accuracy in a small package. It is the smallest dynamically-tuned gyroscope (DTG) produced and offers high performance, small size, excellent reliability and low cost. The G-2000 provides high accuracy for stabilization and
- Angular / Rotary Axes: Biaxial, Triaxial
- Angular Rate Range: 60 to 285 deg/sec
- Operating Temperature: -40 to 185 F
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Supplier: Xsens Technologies BV
Description: will be correct even under accelerations and magnetic distortions. XKF3i comes with several filter setting profiles that are tuned for specific conditions and environments. Hardware design The MTi 10-series is available in two distinctive form factors. The encased version, with its IP
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Supplier: Xsens Technologies BV
Description: will be correct even under accelerations and magnetic distortions. XKF3i comes with several filter setting profiles that are tuned for specific conditions and environments. Hardware design The MTi 10-series is available in two distinctive form factors. The encased version, with its IP
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Supplier: Xsens Technologies BV
Description: will be correct even under accelerations and magnetic distortions. XKF3i comes with several filter setting profiles that are tuned for specific conditions and environments. Hardware design The MTi 10-series is available in two distinctive form factors. The encased version, with its IP
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Supplier: Xsens Technologies BV
Description: will be correct even under accelerations and magnetic distortions. XKF3i comes with several filter setting profiles that are tuned for specific conditions and environments. Hardware design The MTi 10-series is available in two distinctive form factors. The encased version, with its IP
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Inertial measurement unit calibration using Full Information Maximum Likelihood Optimal Filtering
Dynamically tuned gyros (Figure 2-4) are the most common form of free gyros.
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A comparison of multivariable design methodologies for a two-degree-of-freedom gyro torque-rebalance loop
Multivariable design methodologies are compared in the context of controller design for the torque-rebalance loop for a strapdown two-degree-of-freedom dynamically tuned gyro described by complex coefficient differential equations.
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Modeling the dynamically tuned gyroscope in support of high-bandwidth capture loop design
PHYSICS OF THE DYNAMICALLY TUNED GYRO .
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Enhanced precision pointing jitter suppression system
DTG - Dynamically Tuned Gyro ADS - Angular Displacement Sensor .
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Application of Roll-Isolated Inertial Measurement Units to the Instrumentation of Spinning Vehicles
RIMS II: -- Incosym Mod IIIE dynamically tuned gyros (DTGs), Sundstrand QA 1200 accelerometers.
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Fault-tolerant spacecraft attitude control system
Also an optimum symmetrically skewed configuration for the attitude reference system using dynamically tuned gyros is developed.