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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
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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
- 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
- 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: Northrop Grumman Corporation
Description: The LN-120G is a Stellar-Inertial-GPS navigation system that provides precise navigation and sensor pointing with or without GPS. This system integrates stellar tracking and SAASM (Selective Availability Anti-Spoofing Module)-based GPS with a Zero-Lock™ Gyro
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Supplier: Tronics Microsystems
Description: Tronics is the only provider of both closed-loop digital MEMS Accelerometers and Gyros, taking MEMS inertial sensors to an unrivalled level of performance. Closed-loop electronics, also called force-rebalance, brings several key advantages to inertial sensors, including
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Supplier: LORD MicroStrain Sensing Systems
Description: algorithm produces highly accurate computed outputs under dynamic conditions. Computed outputs include pitch, roll, yaw, heading, position, velocity, and GNSS outputs- making it a complete GNSS/INS (GNSS Aided Inertial Navigation System) solution. The use of Micro-Electro-Mechan
- Additional Outputs: Magnetic Field (Magnetometer)
- Angular Rate Range: 300 deg/sec
- Bandwidth: 250 Hz
- Electrical Output: Serial / Digital
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Supplier: LORD MicroStrain Sensing Systems
Description: The 3DM-GX4-45™ is a miniature, industrial-grade GPS Aided Inertial Navigation System (GPS/INS), utilizing the highest performance MEMS sensor technology. It combines a triaxial accelerometer, triaxial gyro, triaxial magnetometer, temperature sensors, pressure altimeter,
- Additional Outputs: Magnetic Field (Magnetometer)
- Angular Rate Range: 300 deg/sec
- Bandwidth: 500 Hz
- Electrical Output: Serial / Digital
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Supplier: Northrop Grumman Corporation
Description: The LN-200S inertial fiber-optic gyro for space applications offers outstanding accel/gyro bias and random walk performance. The LN-200S is a small, lightweight, highly reliable, state-of-the-art fiber-optic inertial measurement unit (IMU). The LN-200S comprises
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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: Northrop Grumman Corporation
Description: /stabilizati on system for ground-based and marine military applications. The LN-270 combines a high accuracy, integrated fiber-optic gyro (FOG), an INS, and a 12-channel P(Y) code GPS. The non-dithered inertial sensor achieves the most precise pointing information
- Angular Rate Range: 1000 deg/sec
- Linear Acceleration Range: 13 +/-g
- Operating Temperature: -65.2 to 160 F
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Supplier: Northrop Grumman Corporation
Description: System and module BIT history storage LTN-101 FLAGSHIP™ Technology FLAGSHIP's™ performance and reliability are based on a series of design innovations: Four Mode Laser Gyro (FLAG) The patented FLAG combines two 18 cm Zero-lock™ Laser
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Supplier: Xsens Technologies BV
Description: possibilities of the MTi, and the integration possibilities of the MT with your own system. With the Development Kit you have will have your measurement unit up and running in just a few minutes to start your first R&D. Highlights 3 products: MTi-10 IMU, MTi-20 VRU and
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Supplier: Xsens Technologies BV
Description: possibilities of the MTi, and the integration possibilities of the MT with your own system. With the Development Kit you have will have your measurement unit up and running in just a few minutes to start your first R&D. Highlights 3 products: MTi-10 IMU, MTi-20 VRU and
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Supplier: Xsens Technologies BV
Description: possibilities of the MTi, and the integration possibilities of the MT with your own system. With the Development Kit you have will have your measurement unit up and running in just a few minutes to start your first R&D. Highlights 3 products: MTi-10 IMU, MTi-20 VRU and
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Supplier: SBG Systems SAS
Description: -effective alternative to FOG technology for mobile land equipment orientation & stabilization such as antenna, targeting systems, gyro stabilized camera, etc. Aerospace IP68 and temperature calibrated from -40° to 75°C, Ekinox-A is designed for harsh environments, and
- 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: iXblue
Description: Advans Vega is a high grade Fiber Optical Gyros Navigation Systems for land applications requiring mobility and accuracy: artillery launchers, antiaircraft systems, surveillance or counterbattery radars, forward observers, reconnaissance vehicles, weapon carriers, tanks
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Supplier: Xsens Technologies BV
Description: possibilities of the MTi, and the integration possibilities of the MT with your own system. With the Development Kit you have will have your measurement unit up and running in just a few minutes to start your first R&D. Highlights 3 products: MTi-10 IMU, MTi-20 VRU and
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Supplier: Tronics Microsystems
Description: verification of the sensor’s integrity and continuous in-operation functionality test. MEMS gyros for navigation of dynamic applications GYPRO®4300 is a high stability MEMS gyro tailored to GNSS-assisted inertial navigation and positioning of ground vehicles
- Angular / Rotary Axes: Uniaxial
- Angular Rate Range: 300 deg/sec
- Bandwidth: 200 Hz
- Bias Stability: 0.4000 deg/hr
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Supplier: Shenzhen Rion Technology Co., Ltd
Description: GI550 MEMS IMU is a tactical-level inertial and integrated navigation system built by the company, which is calibrated precisely in full temperature range to meet the performance requirements under different conditions. The data fusion is realized by the built-in navigation
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Description: in-depth examination of the subtleties, common pitfalls, and limitations of estimation theory as it applies to real-world situations. They present many illustrative examples including adaptations for nonlinear filtering, global navigation satellite systems, the error modeling of
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Supplier: Aerotech, Inc.
Description: testing of space-based sensors in a vacuum and angular testing of inertial sensors such as gyros, MEMS, accelerometers and inertial reference units. The AMG gimbal design incorporates recent Aerotech rotary stage design improvements to provide high performance at
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Supplier: Aerotech, Inc.
Description: sensors in a vacuum and angular testing of inertial sensors such as gyros, MEMS and accelerometers. The AMG LP gimbal design incorporates recent Aerotech rotary stage design improvements to provide high performance at an affordable price. The finest quality motors,
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Supplier: Linde North America, Inc.
Description: commercial, space and military guidance, navigation and control systems. The Ring Laser Gyros (RLG) can be used as the stable elements (for one degree of freedom each) in an inertial guidance system. The advantage of using a RLG is that there are no moving
- Composition: Pure Gas
- Concentration: 99.99 %
- Noble Gases: Neon
- Product Forms: Gas
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Supplier: Tronics Microsystems
Description: The unrivalled noise level and excellent bias stability make AXO®305 an industry-leading sensor solution to build IMU (Inertial Measurement Unit), MRU (Motion Reference Unit), GNSS-aided positioning, navigation, precision attitude, motion control and tilt measurements
- Acceleration: 5 g
- Device Type: Sensor / Transducer
- Features: Self Test / Diagnostics / Self Calibrating
- Frequency Range: 120 Hz
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Supplier: Richardson RFPD
Description: Authentication and Brand protection secure solution with STSAFE-A110 (footprint) Wide range of industrial IoT sensors: – ultra-wide bandwidth (up to 6 kHz), low-noise, 3-axis digital vibration sensor (IIS3DWB) – 3D accelerometer + 3D Gyro iNEMO inertial measurement unit
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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 Inertial Measurement Units (IMU) Datasheets for Tronics Microsystems -
-performance IMU (Inertial Measurement Units) and INS (Inertial Navigation Systems). Click here to learn more and contact us about your next marine or subsea project. (read more)
Browse Accelerometers Datasheets for Tronics Microsystems -
Miniature and robust gyro for systems operating under vibration conditions (read more)
Browse Gyroscopes Datasheets for Tronics Microsystems -
-lead package that ensures long operational and storage life. Its small form-factor allows to build compact multi-axis inertial systems that fit into a low-diameter cylinder. To minimize mechanical cross-coupling effects, GYPRO4300 is available in 3 frequency ranges. Low-SWaP, cost (read more)
Browse Gyroscopes Datasheets for Tronics Microsystems -
Miniature MEMS accelerometers and gyros can be combined into a compact Inertial Measurement Unit (IMU) (read more)
Browse Inertial Measurement Units (IMU) Datasheets for Tronics Microsystems -
. Its bias Instability of 4 μg and bias over temperature of ±0.5 mg enable precise GNSS-aided navigation of manned and unmanned ground vehicles when integrated into an Inertial Navigation System (INS). In subsea environments where satellite-based positioning is not available (read more)
Browse Accelerometers Datasheets for Tronics Microsystems -
μg with a ±0.5 mg bias over its temperature range, thus enabling precise GNSS-aided navigation of manned and unmanned ground vehicles and trains when integrated into Inertial Navigation System (INS). AXO305 is a perfect candidate for Motion Reference Units (MRU) used (read more)
Browse Accelerometers Datasheets for Tronics Microsystems
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Customized Servo Motors Position Gyro-Stabilized Sensor Platform
The best camera and sensor systems in the world are nothing if they're not placed on a stable platform that can point them in the desired direction. No company understands that better than surveillance specialist Gyrocam Systems, LLC (Sarasota, FL), which has developed a gyro-stabilized, servo
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INS600 RTK INTEGRATED NAVIGATION SYSTEM
Kalman filter fusion algorithm is realized by a built-in navigation computer, and outputs real-time accurate carrier posture, heading information, three-dimensional position and velocity information, and various inertial device information. The appearance is exquisite, the structure is small
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Avionics Navigation Systems 2nd Edition Complete Document
The dynamics relating inertial system gyro drift rate equivalent errors to the observable 1/; vector error in this case clearly becomes highly complex and disallows effective calibration using conventional ad hoc fixed gain methods of the early 1960s.
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Trends in inertial systems technology for high accuracy AUV navigation
The sensitivity of performance to the inertial system accuracy was also investigated y increasing the inertial system gyro and accelerometer correlated noise levels to .004 "/hr and 5 pg (lo) respectively, and doubling the gyro random walk to .001 Oldhr. he 10 …
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Back cover
Riscbel, Raymond T-AC 75 Apr 241-244 (IE08) Jump resonance n o h e a r systems; portion of input-output transfer characteristic disjoint from main body: inertial gyro systems .
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Target Design Based Upon Multidisciplinary Uncertainty Information
InField Referencing MWD with advanced magnetic correction + Inertial gyro system Notice that all surveys need a verification survey for the error models to be valid.
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Journal of Jet Propulsion > Advertisment
Rocket guidance systems—such as inertial gyro systems , control systems — actuators and mechanisms, and rocket launching and guidance computers are among the activities currently being car- ried out at the company's Long Island City Plant.
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Integration of Real and Virtual Tools for Suspension Development
Dynamic Data Measurement The test vehicle was instrumented with about 80 channels of data acquisition to measure ride and handling data using sensors such as accelerometers (at axle, chassis, CG), wheel force transducers, inertial gyro system , wheel to body displacement, vehicle slip …
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http://eprints.lancs.ac.uk/42389/1/DavidMolyneaux_PhDThesis.pdf
Similarly, inertial systems ( gyros and accelerometers) are expensive and again subject to drift over time [Lepetit and Fua 2005].
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An economical and highly accurate attitude and position determination system for airborne polarimetric sensors
The GPS APDSsystem offers a cost efficient means of obtaining accurate attitude and position information on aircraft platforms that do not house the latest inertial gyro systems .
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Main braking phase for a soft moon landing as a form of trajectory correction
—Errors in the knowledge of the initial orientation of gyro inertial system relative to the gravitational ver tical (15′).
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Civil Avionics Systems
The inertial sensors located on the stable platform preserve their orientation in space and are: • X accelerometer X gyro • Y accelerometer Y gyro • Z accelerometer Z gyro Inertial systems have the advantage that they are very accurate in the …