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Supplier: MTC Industries & Research Carmiel Ltd.
Description: Miniature, light-weight, precision vertical gyro, designed for use in aircraft, target drones, UAV and stabilized camera platforms The vertical gyro measures roll and pitch. DC input with internal AC inverter to gyro spin motor and erection system. Potentiometer
- Angular / Rotary Axes: Biaxial
- Linearity: 1 ±% Full Scale
- Maximum Dimension: 123 inch
- Operating Temperature: -30 to 70 F
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Supplier: Mid-Continent Instruments and Avionics
Description: Vertical Gyro Remote Manufactured by Collins
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Supplier: Mid-Continent Instruments and Avionics
Description: Vertical Gyro Remote Manufactured by Collins
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Supplier: Mid-Continent Instruments and Avionics
Description: Vertical Gyro Remote Manufactured by Sperry
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Supplier: Mid-Continent Instruments and Avionics
Description: Vertical Gyro Remote Manufactured by Collins
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Supplier: Shenzhen Rion Technology Co., Ltd
Description: TL766D is RION company newly developed three axis angle instrument based on latest MEMS inertial measurement platform , it can simultaneously output Moving carrier’s horizontal angle, vertical angle and horizontal azimuth. The internal integration of the triaxial accelerometer and
- Angular / Rotary Axes: Triaxial
- Angular Rate Range: 300 deg/sec
- Electrical Output: Pulse / Frequency
- Operating Temperature: -40 to 85 F
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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,
- 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: LORD MicroStrain Sensing Systems
Description: The 3DM-GX4-15™ is a miniature high end industrial Inertial Measurement Unit (IMU), utilizing the highest performance MEMS sensor technology. It combines a triaxial accelerometer, triaxial gyro, temperature sensors, pressure altimeter and dual on-board processors running a sophisticated
- Additional Outputs: Magnetic Field (Magnetometer)
- Angular Rate Range: 300 deg/sec
- Bandwidth: 500 Hz
- Electrical Output: Serial / Digital
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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
- Additional Outputs: Magnetic Field (Magnetometer)
- Angular Rate Range: 50 to 1200 deg/sec
- Bandwidth: 225 Hz
- Electrical Output: Serial / Digital
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Supplier: Xsens Technologies BV
Description: _vel 3D (free) acceleration, 3D rate of turn, 3D magnetic field Sensor Component Readout (2 kHz), including (gyro) temperatures Detailed status word Various time stamps
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Supplier: Xsens Technologies BV
Description: _vel 3D (free) acceleration, 3D rate of turn, 3D magnetic field Sensor Component Readout (2 kHz), including (gyro) temperatures Detailed status word Various time stamps
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Supplier: Accuris
Description: VERTICAL GYRO\HONEYWELL INC\VERTICAL GYRO
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Supplier: Accuris
Description: GYRO, VERTICAL AND MOUNT
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Supplier: Accuris
Description: PROPOSED VERTICAL GYRO TEST INSTRUCTIONS
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Supplier: Accuris
Description: GYRO, VERTICAL AND MOUNT (TYPE MF-1 COMPASS)
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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
- Accuracy: 0.0500 ±% Full Scale
- Angular Rate Range: 400 deg/sec
- Bandwidth: 100 Hz
- Electrical Output: Serial / Digital, Network / Fieldbus Output
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Supplier: Northrop Grumman Corporation
Description: configuration in order to fit old mechanical Vertical Gyros' footprints and to provide ease of installation and fast replacement completely transparent to aircraft functions. The availability of several digital and analog interfaces coupled with high maintainability, demonstrated
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Supplier: ZGC, Inc.
Description: conveniently make the connection you need. Total Cine Control: Gamma, Knee, Black, Master Pedestal, Setup Level, Sharpness, Horizontal Detail Frequency, Horizontal/Vertical Detail Balance, Coring, Noise Reduction 1, Noise Reduction 2, Color Matrix, Color Gain, Color Phase, Master Red Gain,
- Application / Industry: Broadcast
- Camera Function: Video
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Supplier: Beechcraft Corporation
Description: conflicts in terrain. Increased Precision A digital Attitude Heading Reference System (AHRS) and an Air Data Computer (ADC) provide attitude and air data information to the system. AHRS replaces pneumatic gyros by using comparative inputs from GPS, a magnetometer and the air data computer to
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Avionics Navigation Systems 2nd Edition Complete Document
Figure 9.4 Gyro vertical with speed and Earth-rate corrections.
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Effect of the inertial accelerations on the accuracy of the CHEKAN-AM gravimeter
where Ti are the time constants of the gyro vertical ;g is the acceleration of gravity; and p is the Laplace operator.
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ARS Journal > Inertial Method of Velocity Measurement
The accelerometers are connected in series with integrators in a torque-transducer circuit, and comprise an integral-control vertical correction network, resulting in a gyro vertical with integral correction, having the same properties as a regulator type of automatic control system.
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Application of a ring laser for measurement of track geometrical parameters
… Equations (1 ..3), in order for the angles K, 0, y to be determined, it is necessary that the system of three nonlinear differential equations should be integrated, thus, we will obtain a strapdown attitude orientation system or full analytical gyro vertical .
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Theoretical physics 1
When I1 = I2 is the moment of inertia for rotations about an axis therefore that passes through S and perpendicularly stands on the figure axis of the gyro , the set then applies the section 3.5 after the Steiner ' Chen to …
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Development of a gyro stabilization system with fiber-optic gyroscopes for an air-sea gravimeter
The loop for AC signal generation shown in Fig. 2 gives the gyrostabilizer properties of a short period gyro vertical damped with the use of velocity measure ments.
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ARS Journal > Contribution to the Theory of Inertial Damped Systems With Arbitrary Period, Invariant With Respect to Maneuvering of the Object
We denote by a and /5 small deflections of the gyro vertical from the local vertical, along the x and y axes, respectively, and by Vx and Vv the components of the inertial velocity of the object.
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Direct Recovery of Deflections of the Vertical Using an Inertial Navigator
each gyro Vertical gyro .