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Supplier: Mid-Continent Instruments and Avionics
Description: Turn Coordinator 12â€"32V Manufactured by Mid-Continent Instruments and Avionics
- Gyro Type: Rate Gyro
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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 in-run
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Supplier: Shenzhen Rion Technology Co., Ltd
Description: North finder is mainly used to find true north automatically. After get heading angle, if north finding inertial navigation start to move, it could output continuous changing dynamic tilt angle and heading angle. Polaris-II uses low speed drift MEMS gyro to find north, built-in IMU is used to
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Supplier: Newark, An Avnet Company
Description: CRM100 gyro eval board
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Supplier: Mid-Continent Instruments and Avionics
Description: Turn Coordinator 11â€"32V, Autopilot, KAP 140 Manufactured by Mid-Continent Instruments and Avionics
- Gyro Type: Rate Gyro
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Supplier: Mid-Continent Instruments and Avionics
Description: Turn and Bank Indicator 12â€"32V, 3-pin, White ball Manufactured by Mid-Continent Instruments and Avionics for Cessna
- Gyro Type: Rate Gyro
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Supplier: Mid-Continent Instruments and Avionics
Description: Turn Coordinator 11â€"32V, Lighted, Brushless Manufactured by Mid-Continent Instruments and Avionics
- Gyro Type: Rate Gyro
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Supplier: Northrop Grumman Corporation
Description: The LN-100G is a versatile Inertial Navigation System/Global Positioning System (INS/GPS) capable of performing high-accuracy navigation while supplying unsurpassed sensor stability for superior geo-location needs. The LN-100G is a non-dithered 0.8 nm/hr free INS/GPS utilizing the Zero-Lock™
- Angular Rate Range: 400.0000000000002 deg/sec
- Linear Acceleration Range: 16 g
- Operating Temperature: -65.2 to 159.8 F
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Supplier: Newark, An Avnet Company
Description: MEMS DEV, AEC-Q100, GYRO/ACCELEROMTR, LGA ROHS COMPLIANT: YES
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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 three solid-state
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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 (ZLGTM) inertial system to provide
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Supplier: Northrop Grumman Corporation
Description: 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 FOG technology eliminates
- Angular Rate Range: 1,000.000000000002 deg/sec
- Linear Acceleration Range: 28 g
- Operating Temperature: -65.2 to 159.8 F
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Supplier: PCB Piezotronics, Inc.
Description: RATE SENSOR
- Output Options: Analog Voltage
- Gyro Type: Rate Gyro
- Angular / Rotary Axes: Uniaxial
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Supplier: Minka Group
Description: VintageGyro; 100 Mini-Can Halogen
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Supplier: Minka Group
Description: VintageGyro; 100 Mini-Can Halogen
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Supplier: Acme Chip Technology Co., Limited
Description: SENSOR GYRO 100DEG SNGL AXIS SPI
- Operating Temperature: -40 to 257 F
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Description: GYRO 100DEG/S 10MV 28LGA
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Supplier: TE Connectivity
Description: Sensor Type : Rate Sensors/Gyros Usage Conditions Operating Temperature Range : -40 - 105 DEGC [-40 - 221 DEGF ]
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Supplier: Minka Group
Description: Gyro; 1-100W Mini-Can Halogen; Sterling Walnut; Matching Glass Shade; 42"Dia
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Supplier: Minka Group
Description: Gyro; 1-100W Mini-Can Halogen; Belcaro Walnut; Matching Glass Shade; 42"Dia
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Supplier: Transcat, Inc.
Description: Product Highlights 3/8"Drive 1200 in-lb Electronic Torque & Angle Wrench. 60-1200 in-lb, 5-100 ft-lb, 6.78-135 Nm Torque and Angle function simultaneously Instant gyro-synchronization when wrench is turned on and ready to use ±1% Accuracy of reading 10 to 100% of scale in both CW & CCW
- Torque: 1,200 In-lbs
- Type: Torque Wrench
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Supplier: Transcat, Inc.
Description: Product Highlights 3/8 Drive, Torque & Angle Meter, Range 48-1200 in-lb, 4-100 ft-lb, 6-135 Nm Eliminates hand held position error ±1% Accuracy of reading 10 to 100% of scale in both directions (Clockwise & Counter Clockwise) Instant Gyro Synchronization ±1° Precision at normal speed of
- Maximum Torque: 1,200 In-lbs
- Category of Device: Instrument / Meter
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Supplier: Transcat, Inc.
Description: Product Highlights 3/8 Drive, Torque & Angle Meter, Range 60-1200 in-lb, 5-100 ft-lb, 6.78-135 Nm Eliminates hand held position error ±2% Accuracy of reading 10 to 100% of scale in both directions (Clockwise & Counter Clockwise) Instant Gyro Synchronization ±1° Precision at normal speed of
- Maximum Torque: 1,200 In-lbs
- Category of Device: Instrument / Meter
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Supplier: Shenzhen Rion Technology Co., Ltd
Description: technology , according to the user needs, to keep the user's parameters after power off can still remember, in favour of user's secondary development. Intergrated nine axis sensor and temperautre sensor Multiple intelligent acceleration and gyro cross interference algorithm High performance
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Supplier: Transcat, Inc.
Description: Product Highlights 1/4"Drive 250 in-lb Electronic Torque & Angle Wrench. 12.5-250 in-lb, 1-20.7 ft-lb, 1.3-28 Nm Torque and Angle function simultaneously Instant gyro-synchronization when wrench is turned on and ready to use ±1% Accuracy of reading 10 to 100% of scale in both CW & CCW
- Torque: 250 In-lbs
- Type: Torque Wrench
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Supplier: ValueTronics International, Inc.
Description: applications as well as for Automatic Test Equipment systems and avionics testing. Power fault simulation when used with an Elgar Plug-In Programmer Frequency conversion (60 to 50 Hz or 50 to 60 Hz) for generating international or USA power Power supply testing Gyro testing Avionics testing
- Type: AC Power Source
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Supplier: ValueTronics International, Inc.
Description: protection helps prevent damage to the Valhalla 2300 3 Phase Digital Power Analyzer. It can withstand a max. of 500% overload on current (ie 500 amps on the 100 amp range) and up to 3000, V pk-pk of voltage without any problems. For dedicated low voltage applications, such as three phase gyro
- Electrical Parameters: AC Voltage
- Phase: Three-Phase
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Supplier: Xsens Technologies BV
Description: angles, quaternions, matrix) 3D delta_q and 3D delta_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: angles, quaternions, matrix) 3D delta_q and 3D delta_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: Airbus Group
Description: payload concept: DVF 2000 has a plug-and-play interface that allows rapid integration of custom payloads. The payload (daylight or infrared camera) is integrated in a gyro-stabilized gimbal, which reduces the impact of aircraft movement. This allows the operator to steadily point to the
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Supplier: Xsens Technologies BV
Description: angles, quaternions, matrix) 3D delta_q and 3D delta_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: Cessna Aircraft Company
Description: GMU-44 Magnetometer Garmin SafeTaxi & FliteCharts Electronic Checklists Emergency Locator Transmitter Remote Mounted Switch Backup Attitude Gyro, Altimeter, and Airspeed Indicator Control Wheel Push-To-Talk Switch-Pilot/Copilot Mic & Phone Jacks — Pilot/Copilot/Passengers Auxiliary Stereo
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Sensor integration in airborne mapping
… lock™ Laser Gyro (ZLG™) and A-4 accelerometer triad (0.8 nmi/h CEP, gyro bias—0.003 /h … The LN100 firmware, modified for the AIMS™ project, allows for access to the raw IMU data, updated …
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A new integrated optical angular velocity sensor
S. J. Sanders, L. K. Strandjord, D. Mead, “Fiber optic gyro technology trends - a Honeywell perspective”, Optical … … gg1305an.htm 11. http://www.ngnavsys.com/Html/LN-100LG/ 12. http://www.aselsan.com.tr/mging/products/ ln100 .htm 13.
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First flights of a new airborne thermal infrared imaging spectrometer with high area coverage
The whole sensor assembly sits on a 3-axis, gyro -stabilized mount that greatly reduces both low … The 3-axis stabilization platform (Intergraph Z/I mount), inertial navigation system (Litton LN100 -G) and calibration sources …
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http://dspace.mit.edu/bitstream/handle/1721.1/74140/2-017j-spring-2006/contents/lecture-notes/18navigation.pdf
Gyro measurements The Litton LN100 alone achieves ~1mile/hr drift; depends strongly on errors in initialization.
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TIER II Plus airborne EO sensor LOS control and image geolocation
alsohas the capacity to attenuate any gyro or IMC loop dynamicsthrough transfer function cancellationtechniques. Most of the inputs required for command generation are provided by the LN100 GPS / INS.
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GPS error modeling and OTF ambiguity resolution for high-accuracy GPS/INS integrated system
Gyro errors (random walk) Drifts … implemented in the integrated ®lter are reliable, since they were suggested by the LN100 manufacturer, based on …
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http://dspace.mit.edu/bitstream/handle/1721.1/16676/56844726-MIT.pdf?sequence=2
Value Gyro Accuracy It contains a reference solution that was computed by an onboard Litton LN100 , which is a full …
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Applied Mechanics and Mechanical Engineering III
… Bu Ji-jun, Wei Gui-ling and Li Yong-jian: Two-Position Detecting Scheme for Gyro -Based ln100 − ln φ − ln Pg + 14.4351 .
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Lightweight GNSS/IRS integrated navigation system for UAV vehicles
3 Gyros [3] C. Jekeli “Algorithms and Preliminary Experiences with the LN93 and LN100 for Airborne Vector Gravimetry” Air …
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Intelligent Data Engineering and Automated Learning - IDEAL 2009
1+ ln100 (a) Satellite gyro failure prediction.
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