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Supplier: Gladiator Technologies, Inc.
Description: G150Z Gyro represents Gladiator's breakthrough gyro technology enabling an ultra low noise MEMS gyro and bandwidth of 200Hz that has performance commensurate with much more expensive small RLG's and small open loop FOG's. The G150Z also features industry leading bias
- Angular / Rotary Axes: Uniaxial
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Supplier: Northrop Grumman Corporation
Description: The Northrop Grumman Italia LISA-200 AHRS, is a lightweight Fiber Optic Gyroscope Attitude Heading Reference System (FOG AHRS) based on a state-of-art Northrop Grumman LN-200 Inertial Measurement Unit and Northrop Grumman Italia's 20 years of experience in the design, development, and
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Supplier: Tronics Microsystems
Description: High stability and repeatability for navigation in severe temperature and vibrations conditions GYPRO®4300 is a high-performance, closed-loop digital MEMS gyroscope with ± 300 °/s input range that offers a cost-effective alternative to Fiber-Optic Gyroscopes (FOG
- Angular / Rotary Axes: Uniaxial
- Angular Rate Range: 300 deg/sec
- Bandwidth: 200 Hz
- Bias Stability: 0.4000 deg/hr
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Supplier: SBG Systems SAS
Description: Web Interface >48h Internal Data Logger Robust IP68 Aluminum Enclosure Ekinox Series Brings Robust and Cost-effective MEMS to FOG Level Ekinox Series brings robust, maintenance free, and cost-effective MEMS to the Fiber Optic Gyro accuracy and
- Angular / Rotary Axes: Triaxial
- Angular Rate Range: 400 deg/sec
- Bandwidth: 100 Hz
- Bias Stability: 3 deg/hr
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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 for increased sensor
- 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: Grumman Awarded U.S. Military Contract for Navigation Systems The LN-260 is a high performance, low cost INS/GPS that utilizes the state-of-the-art fiber-optic gyroscope (FOG)-based inertial navigation sensor assembly with 24 channel Selective Availability Anti-Spoofing Module (SAASM) GPS.
- Operating Temperature: -40 to 160 F
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Supplier: Northrop Grumman Corporation
Description: INS/GPS has various advantages, including light weight, low cost and high performance. The LN-251 fiber-optic gyro (FOG) employs one of our most modern technologies and includes three independent navigation solutions: blended INS/GPS, INS-only, and GPS-only. The non-dithered, low noise
- Angular Rate Range: 1000 deg/sec
- Linear Acceleration Range: 28 +/-g
- Operating Temperature: -65.2 to 160 F
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Supplier: Cessna Aircraft Company
Description: , and more. The G1000 flight deck is standard on our Caravan and Citation Mustang models as well, so your transition between aircraft will be smoother when you upgrade. Virtual landscapes Synthetic Vision Technology enhances visual orientation in darkness, fog, haze, rain or any solid
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Supplier: Cessna Aircraft Company
Description: -dimensional renderings of terrain on both flight displays. You’ll feel confident in darkness, haze, rain, fog, or any other IFR conditions that might obstruct a clear view through the windshield. This advanced graphics modeling technology recreates the surrounding landscape accurately in
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miniature package and low-power consumption, Tronics GYPRO4300 gyro offers a digital, cost-effective, and low-SWaP alternative to bulky, expensive, and power-consuming solutions like DTG (Dynamically Tuned Gyros) FOG (Fiber Optical Gyroscopes). Due to its solid-state architecture that reduces (read more)
Browse Gyroscopes Datasheets for Tronics Microsystems -
Discover our GYPRO4300, a high-performance, closed-loop digital MEMS gyroscope with ± 300 °/s input range that offers a cost-effective alternative to Fiber-Optic Gyroscopes (FOG) at a fraction of their size, weight, and power consumption. (read more)
Browse Gyroscopes Datasheets for Tronics Microsystems -
-effective and high reliability gyroscope Thanks to its miniature package and low-power consumption, Tronics GYPRO4300 gyro offers a digital, cost-effective, and low-SWaP alternative to bulky, expensive, and power-consuming solutions like DTG (Dynamically Tuned Gyros) and FOG (Fiber Optical (read more)
Browse Gyroscopes Datasheets for Tronics Microsystems -
quartz accelerometers and FOG gyros. They significantly demonstrate excellent performances under severe temperature and vibrations conditions at a fraction of their size, weight, and power consumption. To optimize the UAV's payload, Tronics' high-performance MEMS inertial sensors are packed (read more)
Browse Accelerometers Datasheets for Tronics Microsystems -
Are you involved in the design of trainborne positioning and navigation systems ? Discover AXO®305, a ± 5 g high precision digital MEMS accelerometer and GYPRO®4300, a ± 300 °/s high stability digital MEMS gyro that demonstrate (read more)
Browse Accelerometers Datasheets for Tronics Microsystems -
bias instability and Angular Random Walk (ARW) to ensure accurate azimuth angle measurement. High-performance digital MEMS gyros and accelerometers offer a low-cost and low-SWaP alternative to the bulky and expensive quartz and FOG sensors utilized in the oil and gas (read more)
Browse Inertial Measurement Units (IMU) Datasheets for Tronics Microsystems -
precision guidance, navigation, and dynamic positioning functions. High performance digital MEMS accelerometers and gyros are a cost-effective and low-SWaP alternative to bulky and costly quartz, FOG and DTG originally used in marine and (read more)
Browse Inertial Measurement Units (IMU) Datasheets for Tronics Microsystems -
, low-SWaP and cost-effective alternative to bulky and expensive analog quartz accelerometers and FOG (Fiber Optic Gyros), demonstrating challenging performances at a fraction of their price, size and power consumption (read more)
Browse Inertial Measurement Units (IMU) Datasheets for Tronics Microsystems
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Future evolution of fiber optic gyros
Fiber optic gyros ( FOGs ) have been studied over the past 20 years.
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Environmental Performance Of Attitude And Heading Reference Grade Fiber Optic Rotation Sensors
During the past 17 years, worldwide interest in fiber optic gyros ( FOGs ) has prompted considerable development of this new family of rotation sensors** .
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Fiber Optic Gyroscope Review And Market Forecast
the next decade, fiber optic gyro ( FOG ) production will expand impressively, reaching $125 million* in 1994.
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Fiber Optic Angular Rotation Sensor Market Forecast
Over the next decade, fiber optic gyro ( FOG ) production will expand impressively, reaching $125 mil- lion* in 1994.
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Progress in fiber optic gyro development and application
Single-axis fiber-optic gyro ( FOG ) basic designs can be considered as complete.
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The influences of the gyro sensors' errors on the attitude calculus
The first gyro is a MEMS whose functioning is based on the Coriolis forces, the second one is a fiber optic gyro ( FOG ) while the third one is a laser gyro.
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General formula describing drift of interferometer fiber-optic gyro due to Faraday effect: reduction of the drift in twin-depo-I-FOG
Index Terms—Degree of depolarization, Faraday effect, fiber- optic gyro ( FOG ), optical fiber sensor, state of polarization.
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Improving information autonomy of marine SINS
Marine SINS are designed on more accurate navi gation grade gyros: Mk49 (Sperry and Honeywell, USA), Sigma 40XP (Sagem, France)) use laser gyros, and PHINS and MARINS (IXblue, France) are built on fiber optic gyros ( FOG ).
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Achievements And Perspectives Of Fiber Gyros
At SEL two types of fiber optical gyros ( FOG ) have been pursued, the phase -modulated and the frequency- modulated FOG (fig. 2.1).
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Y-integrated optic chip (Y-IOC) applied in fiber optic gyro
Its performances have very important influences on fiber optic gyro ( FOG ) accuracies.