Untitled
Abstract: No abstract text available
Text: IMU-3000 Product Specification Document Number: PS-IMU-3000A-00 Revision: 1.3 Release Date: 05/25/2011 IMU-3000 Motion Processing Unit Product Specification Rev 1.3 1 of 42 IMU-3000 Product Specification Document Number: PS-IMU-3000A-00 Revision: 1.3 Release Date: 05/25/2011
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IMU-3000
PS-IMU-3000A-00
IMU-3000
IMU-3000TM,
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systron donner accelerometer
Abstract: mems Gyro missile IMU gyro Inertial system donner LINEAR accelerometer systron donner VIBRATION SENSOR mtbf missile accelerometer mems missile MEMS IMU
Text: DQI Digital Quartz IMU Inertial Measurement Unit Applications Physical Characteristics System Performance Environmental High-Performance, Low-Cost INS Technology The DQI, or Digital Quartz IMU (Inertial Measurement Unit), is a powerful component of BEI Systron Donner Inertial Division's technology solutions - offering "Six Degrees of Freedom"
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CLM-112-02-LM-D-A
Abstract: MEMS IMU mems gyroscope looney tunes ADSP-BF533 AN-1041 adisusbz output data bartlett window three axis gyroscope ADIS1640X
Text: AN-1041 APPLICATION NOTE One Technology Way • P.O. Box 9106 • Norwood, MA 02062-9106, U.S.A. • Tel: 781.329.4700 • Fax: 781.461.3113 • www.analog.com iSensor IMU Quick Start Guide and Bias Optimization Tips by Mark Looney INTRODUCTION The iSensor IMU products include ADIS1636x and ADIS1640x.
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AN-1041
ADIS1636x
ADIS1640x.
AN08403-0-8/09
CLM-112-02-LM-D-A
MEMS IMU
mems gyroscope
looney tunes
ADSP-BF533
AN-1041
adisusbz output data
bartlett window
three axis gyroscope
ADIS1640X
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imu700cb
Abstract: IMU700CB-200 fiber optic gyroscope military IMU 6dof IMU700 IMU7000CB-200 FOG sensor missile gyroscope 9 AXIS mems Gyro missile
Text: IMU700 fiber optic based imu • High Bandwidth Angular Rate and Linear Acceleration Measurement • Fiber Optic Gyro Stability < 20°/hr • Analog and Digital Outputs • No Calibration Required Applications • Control and Stabilization • Avionics • Instrumentation
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IMU700
IMU700CB
IMU700CB
300km
IMU700CB-200
fiber optic gyroscope
military IMU
6dof
IMU700
IMU7000CB-200
FOG sensor missile
gyroscope 9 AXIS
mems Gyro missile
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Untitled
Abstract: No abstract text available
Text: EVALUATION KIT AVAILABLE MAX21100 Low-Power, Ultra-Accurate 6+3 DoF IMU General Description Features and Benefits The MAX21100 is the industry’s most accurate 6+3 DoF inertial measurement unit available in a 3mm x 3mm x 0.83mm package and capable of working with a supply
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MAX21100
MAX21100
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Deutsch DT06-12S
Abstract: No abstract text available
Text: 6DF Series 6 Degrees of Freedom Inertial Measurement Unit, 6-D Motion Variant DESCRIPTION The Honeywell 6-D Motion Variant 6DF six degrees of freedom Inertial Measurement Unit (IMU) sensors are designed to provide motion, position, and navigational sensing
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000741-2-EN
Deutsch DT06-12S
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hmc5883
Abstract: HMC5883L IMU-3000 mems gyroscope three axis Gyroscope technical data mems gyroscope current sensing avr AVR4018 IMU3000 IMU-3000TM
Text: AVR4018: Inertial Two ATAVRSBIN2 Hardware User's Guide Features • • • • • • • Compatible with all Atmel AVR® Xplain MCU boards Full nine-degree-of-freedom inertial sensing InvenSense three-axis MEMS gyroscope (IMU-3000 ) Kionix® three-axis MEMS accelerometer (KXTF9)
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AVR4018:
IMU-3000TM)
HMC5883)
IMU-3000
369A-AVR-01/11
hmc5883
HMC5883L
IMU-3000
mems gyroscope three axis
Gyroscope technical data
mems gyroscope
current sensing avr
AVR4018
IMU3000
IMU-3000TM
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Untitled
Abstract: No abstract text available
Text: One Technology Way • P.O. Box 9106 · Norwood, MA 02062-9106 · Tel: 781.329.4700 · Fax: 781.461.3113 · www.analog.com ADIS16IMU1/PCBZ Breakout Board Wiki-Guide OVERVIEW The ADIS1613x, ADIS1636x, ADIS16375, ADIS16407 and ADIS1648x IMU products all use a 24-pin,
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ADIS16IMU1/PCBZ
ADIS1613x,
ADIS1636x,
ADIS16375,
ADIS16407
ADIS1648x
24-pin,
ADIS16IMU1/PCBZ.
16-pin,
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DMU10-22-0100
Abstract: No abstract text available
Text: DMU10 Technical Datasheet Six Degrees of Freedom Precision MEMS Inertial Measurement Unit www.siliconsensing.com DMU10-01 DMU10-02 OEM Module Features 1 General Description • High performance six degrees of freedom 6-DOF MEMS IMU • 7 sensor inputs - Angular rate (x3)
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DMU10
DMU10-01
DMU10-02
RS-422
DMU10-00-0100-132
DMU10-22-0100
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Untitled
Abstract: No abstract text available
Text: Powerful Solutions for a Better Life IMU800 LOW DRIFT MEMS IMU MEMSIC’s IMU800CA establishes a new level of performance for standalone “unaided” inertial systems. The IMU800CA combines advanced MEMS rate gyro and accelerometer technologies to provide a superior solution for six-degree-offreedom measurement in dynamic environments.
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IMU800
IMU800CA
300km
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Untitled
Abstract: No abstract text available
Text: Powerful Solutions for a Better Life IMU800 LOW DRIFT MEMS IMU MEMSIC’s IMU800CA establishes a new level of performance for standalone “unaided” inertial systems. The IMU800CA combines advanced MEMS rate gyro and accelerometer technologies to provide a superior solution for six-degree-offreedom measurement in dynamic environments.
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IMU800
IMU800CA
300km
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bias stability gyro mems
Abstract: No abstract text available
Text: EVALUATION KIT AVAILABLE MAX21100 Low-Power, Ultra-Accurate 6+3 DoF IMU General Description Features and Benefits The MAX21100 is the industry’s most accurate 6+3 DoF inertial measurement unit available in a 3mm x 3mm x 0.83mm package and capable of working with a supply
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MAX21100
MAX21100
bias stability gyro mems
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Untitled
Abstract: No abstract text available
Text: EVALUATION KIT AVAILABLE MAX21100 Low-Power, Ultra-Accurate 6+3 DoF IMU General Description Features and Benefits The MAX21100 is the industry’s most accurate 6+3 DoF inertial measurement unit available in a 3mm x 3mm x 0.83mm package and capable of working with a supply
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MAX21100
MAX21100
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Untitled
Abstract: No abstract text available
Text: 2. Soldering the headers Before using your click board, make sure to solder 1x8 male headers to both left and right side of the board. Two 1x8 male headers are included with the board in the package. MPU IMU click 2 1 3 4. Essential features 1. Introduction
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MPU-6000,
MPU-6000
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Gyroscope
Abstract: Inertial navigation system mems gyro automotive MLX90609-N2 gyroscope ANGLE car navigation system reckoning 10 DOF imu IMU gyro mems gyroscope
Text: High Performance Navigation Systems with Melexis MLX90609-N2 Gyroscope Guido Dupont, Melexis Technologies SA, Switzerland CONFIDENTIA L A ND PROPRIETA RY Copyright 2004 Me lex is Microe le ctronic Integrated Systems. All R ights Rese rve d 1 AMAA - Berlin May 2007
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MLX90609-N2
MLX90609-N2)
MLX90609
Gyroscope
Inertial navigation system
mems gyro automotive
MLX90609-N2
gyroscope ANGLE
car navigation system
reckoning
10 DOF imu
IMU gyro
mems gyroscope
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gyro sensor
Abstract: No abstract text available
Text: MEMS Inertial Measurement Units for Complex Motion Capture and Processing Industrial, healthcare, and military/aerospace designs are increasingly deploying MEMS inertial measurement units IMUs for highly precise control, automation, and positioning applications.
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BR11505-2-5/13
gyro sensor
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3111r
Abstract: DGPS receiver rs232 DGPS IMU gyro 3151R NovAtel 424-RT2W "ring laser" IMU datasheet RT20
Text: 04-013 Page 1 of 7 BULLETIN Introduction of SPAN Technology SPAN Technology NovAtel is pleased to introduce SPANTM Synchronized Position Attitude Navigation Technology, a next generation positioning system that combines GPS and inertial capabilities for uninterrupted operation and
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ADIS16485
Abstract: ADIS16488 adis-16488-amlz UG-287 waveform recorder mini m2 usb 2.0 ADIS16488AMLZ
Text: Evaluation Board User Guide UG-287 One Technology Way • P.O. Box 9106 • Norwood, MA 02062-9106, U.S.A. • Tel: 781.329.4700 • Fax: 781.461.3113 • www.analog.com EVAL-ADIS: iSensor Evaluation System FEATURES PC USB evaluation system for inertial measurement units
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UG-287
ADIS16334,
ADIS16375,
ADIS16485,
ADIS16488
32-bit
64-bit
16-bit
16-pin
UG09902-0-6/12
ADIS16485
adis-16488-amlz
UG-287
waveform recorder
mini m2 usb 2.0
ADIS16488AMLZ
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Untitled
Abstract: No abstract text available
Text: Evaluation Board User Guide UG-287 One Technology Way • P.O. Box 9106 • Norwood, MA 02062-9106, U.S.A. • Tel: 781.329.4700 • Fax: 781.461.3113 • www.analog.com EVAL-ADIS: iSensor Evaluation System FEATURES PC USB evaluation system for inertial measurement units
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UG-287
32-bit
64-bit
ADIS16xxx
16-pin
UG09902-0-2/13
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gyroscopes
Abstract: No abstract text available
Text: Technical Article MS-2432 . The Battle Between MEMS and FOGs for Precision Guidance REAL-TIME NAVIGATION HARDWARE The navigation system used in this work was designed to provide high rate attitude outputs to a motor, which then stabilized an antenna array on the roof of a vehicle. The
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MS-2432
TA11274-0-1/13
gyroscopes
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Specification
Abstract: bias stability gyro mems
Text: DMU30 Technical Datasheet High Performance MEMS Inertial Measurement Unit HPIMU www.siliconsensing.com Applications y Hydrographic surveying Airborne survey and mapping INS (Inertial Navigation Systems) AHRS (Attitude and Heading Reference System) GPS drop-out aiding
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DMU30
DMU30-00-0100-132
Specification
bias stability gyro mems
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Untitled
Abstract: No abstract text available
Text: Technical Article MS-2694 Enabling Next-Generation Avionics Systems by Bob Scannell, business development manager, Analog Devices, Inc. Recent generations of MEMS technology are now providing highly robust, critical performance to avionics equipment, with significant advances in size, weight, power SWAP ,
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MS-2694
TA12652-0-8/14
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Litton LN-200
Abstract: mini helicopter project Tokin CG-16D gyros SRF04 radio controlled helicopter ENC-05E LN-200 TANS III GPS HP54600B uvtron
Text: Bilag 1: Helikopterens fysiske egenskaber Bilag 1: Helikopterens fysiske egenskaber I dette bilag redegøres for Draganflyer III helikopterens fysiske egenskaber såsom dimensioner, vægt og nyttelast. Helikopterens dimensioner er angivet på følgende figur
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RRS01-05
Abstract: No abstract text available
Text: SiRRS01 Family of Sensors ® SiRRS01 Atlantic Inertial Systems’ SiRRS01® was the world’s first silicon micro-machined ring gyroscope. The SiRRS01® angular rate sensor evolved from the highly successful Vibrating Structure Gyroscope developed by Atlantic Inertial Systems, which has been
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SiRRS01
RRS01-05
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