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Supplier: Gladiator Technologies, Inc.
Description: The all new G200 Dual Axis MEMS Gyro represents Gladiator’s breakthrough gyro technology enabling an ultra low noise two axis MEMS gyro and bandwidth of 200Hz that has performance commensurate with much more expensive small Dynamically Tuned Gyros. It alsoShow More
Standards and Technical Documents - 813-1988 - IEEE Specification Format Guide and Test Procedure for Two-Degree-Of-Freedom Dynamically Tuned Gyros -- 10.1109/IEEESTD.1989.94579
Description: Abstract This specification defines the requirements for a two-degree-of-freedom 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.Show More
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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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.
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.
Modeling the dynamically tuned gyroscope in support of high-bandwidth capture loop design
PHYSICS OF THE DYNAMICALLY TUNED GYRO .
Enhanced precision pointing jitter suppression system
DTG - Dynamically Tuned Gyro ADS - Angular Displacement Sensor .
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.
Fault-tolerant spacecraft attitude control system
Also an optimum symmetrically skewed configuration for the attitude reference system using dynamically tuned gyros is developed.