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Analog Devices Inc ADIS16480BMLZ MODULE GYRO/ACCELEROMETER 24LEAD
Distributors	Part	Package	Stock	Lead Time	Min Order Qty	Price	Buy
DigiKey	ADIS16480BMLZ	Box	1		1	1 $3614.86 10 $3614.86 100 $3614.86 1000 $3614.86 10000 $3614.86	Buy Now
Mouser Electronics	ADIS16480BMLZ		6			1 $4022.01 10 $4022.01 100 $4022.01 1000 $4022.01 10000 $4022.01	Buy Now
Verical	ADIS16480BMLZ		122		1	1 $3637.5974 10 $3637.5974 100 $3637.5974 1000 $3637.5974 10000 $3637.5974	Buy Now
Newark	ADIS16480BMLZ	Bulk	1		1	1 $3626.46 10 $3626.46 100 $3626.46 1000 $3626.46 10000 $3626.46	Buy Now
Richardson RFPD	ADIS16480BMLZ				1	1 $3932.97 10 $3733.83 100 $3687.16 1000 $3687.16 10000 $3687.16	Buy Now

Vyrian	ADIS16480BMLZ		25			1 - 10 - 100 - 1000 - 10000 -	Get Quote
Analog Devices Inc ADIS16480AMLZ IMU ACCEL/GYRO/MAG SPI 24ML
Distributors	Part	Package	Stock	Lead Time	Min Order Qty	Price	Buy
DigiKey	ADIS16480AMLZ	Bulk				1 - 10 - 100 - 1000 - 10000 -	Buy Now
Vyrian	ADIS16480AMLZ		877			1 - 10 - 100 - 1000 - 10000 -	Get Quote

ADIS16480 Datasheets (3)

Part	ECAD Model	Manufacturer	Description	Curated	Datasheet Type	PDF
ADIS16480AMLZ		Analog Devices	ADIS16480 - IC SPECIALTY ANALOG CIRCUIT, Analog IC:Other		Original	PDF
ADIS16480BMLZ		Analog Devices	Sensors, Transducers - Motion Sensors - IMUs (Inertial Measurement Units) - MODULE GYRO/ACCELEROMETER 24LEAD		Original	PDF
ADIS16480/PCBZ		Analog Devices	ADIS16480 - Ten Degrees of Freedom MEMS Inertial Sensor with Dynamic Orientation Outputs; No of Pins: 0; Temperature Range: INDUSTRIAL; Container: 1/No packing		Original	PDF

ADIS16480 Datasheets Context Search

Catalog Datasheet	Type	Document Tags	PDF
IMU gy 88 Abstract: extended kalman filter attitude heading reference system algorithm based on the Kalman filter bias stability gyro mems Troubleshooting from analog accelerometers scalar magnetometer extended kalman filter WITH ADIS16480 kalman filter accelerometer speed estimation ekf code speed estimation using ekf Contextual Info: Ten Degrees of Freedom Inertial Sensor with Dynamic Orientation Outputs ADIS16480 Data Sheet FEATURES GENERAL DESCRIPTION Dynamic angle outputs Quaternion, Euler, rotation matrix 0.1° pitch, roll and 0.3° (yaw) static accuracy Triaxial, digital gyroscope, ±450°/sec dynamic range	Original	ADIS16480 ADIS16480 03-28-2012-C 24-Lead ML-24-6) ADIS16480AMLZ ADIS16480/PCBZ ML-24-6 IMU gy 88 extended kalman filter attitude heading reference system algorithm based on the Kalman filter bias stability gyro mems Troubleshooting from analog accelerometers scalar magnetometer extended kalman filter WITH ADIS16480 kalman filter accelerometer speed estimation ekf code speed estimation using ekf	PDF
Contextual Info: Ten Degrees of Freedom Inertial Sensor with Dynamic Orientation Outputs ADIS16480 Data Sheet FEATURES GENERAL DESCRIPTION Dynamic angle outputs Quaternion, Euler, rotation matrix 0.1° pitch, roll and 0.3° (yaw) static accuracy Triaxial, digital gyroscope, ±450°/sec dynamic range	Original	ADIS16480 Conf14 12-07-2012-E 24-Lead ML-24-6) ADIS16480AMLZ ML-24-6 D10278-0-1/14	PDF
IMU gy 88 Abstract: ADIS16480 extended kalman filter WITH ADIS16480 kalman filter accelerometer attitude heading reference system algorithm based on the Kalman filter estimation with extended kalman filter kalman filter C extended kalman filter speed estimation ekf code speed estimation using ekf Contextual Info: Ten Degrees of Freedom Inertial Sensor with Dynamic Orientation Outputs ADIS16480 Data Sheet FEATURES GENERAL DESCRIPTION Dynamic angle outputs Quaternion, Euler, rotation matrix 0.1° pitch, roll and 0.3° (yaw) static accuracy Triaxial, digital gyroscope, ±450°/sec dynamic range	Original	ADIS16480 ADIS16480 ADIS16480AMLZ ADIS16480/PCBZ 24-Lead ML-24-6 ADIS16480/PCBZ IMU gy 88 extended kalman filter WITH ADIS16480 kalman filter accelerometer attitude heading reference system algorithm based on the Kalman filter estimation with extended kalman filter kalman filter C extended kalman filter speed estimation ekf code speed estimation using ekf	PDF
Contextual Info: Ten Degrees of Freedom Inertial Sensor with Dynamic Orientation Outputs ADIS16480 Data Sheet FEATURES GENERAL DESCRIPTION Dynamic angle outputs Quaternion, Euler, rotation matrix 0.1° pitch, roll and 0.3° (yaw) static accuracy Triaxial, digital gyroscope, ±450°/sec dynamic range	Original	ADIS16480 levels14 12-07-2012-E 24-Lead ML-24-6) ADIS16480AMLZ ML-24-6 D10278-0-4/14	PDF
Contextual Info: Ten Degrees of Freedom Inertial Sensor with Dynamic Orientation Outputs ADIS16480 Data Sheet FEATURES GENERAL DESCRIPTION Dynamic angle outputs Quaternion, Euler, rotation matrix 0.1° pitch, roll and 0.3° (yaw) static accuracy Triaxial, digital gyroscope, ±450°/sec dynamic range	Original	ADIS16480 03-28-2012-C 24-Lead ML-24-6) ADIS16480AMLZ ADIS16480/PCBZ ADIS16480/PCBZ ADIS16480AMLZ D10278-0-5/12	PDF
Contextual Info: Tactical Grade, Six Degrees of Freedom Inertial Sensor ADIS16485 Data Sheet FEATURES GENERAL DESCRIPTION Triaxial, digital gyroscope, ±450°/sec dynamic range <±0.05° orthogonal alignment error 6°/hr in-run bias stability 0.3°/√hr angular random walk	Original	ADIS16485 indicato14 12-07-2012-E 24-Lead ML-24-6) ADIS16485AMLZ ML-24-6 D10666-0-5/14	PDF
gyro sensor Contextual Info: 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.	Original	BR11505-2-5/13 gyro sensor	PDF
Contextual Info: 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,	Original	ADIS16IMU1/PCBZ ADIS1613x, ADIS1636x, ADIS16375, ADIS16407 ADIS1648x 24-pin, ADIS16IMU1/PCBZ. 16-pin,	PDF
ADXL377 Contextual Info: MEMS Inertial Sensors Accelerometers Range g Output Type Sensing Axes BW Typ (kHz) Sensitivity Noise (mg/√Hz ) ADXL103 ±1.7, ±18 Analog 1 2.5 100 mV/g to 1000 mV/g ADXL78 ±35, ±50, ±70 Analog 1 0.4 27 mV/g to 55 mV/g ADXL001 ±70, ±250, ±500	Original	ADXL103 ADXL78 ADXL001 ADXL203 ADXL206 ADXL278 ADXL335 ADXL326 ADXL337 ADXL325 ADXL377	PDF
Contextual Info: Tactical Grade, Six Degrees of Freedom Inertial Sensor ADIS16485 Data Sheet FEATURES GENERAL DESCRIPTION Triaxial, digital gyroscope, ±450°/sec dynamic range ±0.05° orthogonal alignment error 6°/hr in-run bias stability 0.3°/√hr angular random walk	Original	ADIS16485 12-07-2012-E 24-Lead ML-24-6) ADIS16485BMLZ D10666-0-2/15 ML-24-6	PDF
Contextual Info: Tactical Grade Ten Degrees of Freedom Inertial Sensor ADIS16488A Data Sheet FEATURES GENERAL DESCRIPTION Triaxial, digital gyroscope, ±450°/sec dynamic range <±0.05° orthogonal alignment error 5.1°/hr in-run bias stability 0.26°/√hr angular random walk	Original	ADIS16488A correc12-07-2012-E 24-Lead ML-24-6) ADIS16488BMLZ ADIS16488CMLZ ML-24-6	PDF
Contextual Info: Tactical Grade, Six Degrees of Freedom Inertial Sensor ADIS16485 Data Sheet FEATURES GENERAL DESCRIPTION Triaxial, digital gyroscope, ±450°/sec dynamic range <±0.05° orthogonal alignment error 6°/hr in-run bias stability 0.3°/√hr angular random walk	Original	ADIS16485 indicato14 12-07-2012-E 24-Lead ML-24-6) ADIS16485AMLZ ML-24-6 D10666-0-4/14	PDF
Contextual Info: Tactical Grade Ten Degrees of Freedom Inertial Sensor ADIS16488 Data Sheet FEATURES GENERAL DESCRIPTION Triaxial, digital gyroscope, ±450°/sec dynamic range <±0.05° orthogonal alignment error 6°/hr in-run bias stability 0.3°/√hr angular random walk	Original	ADIS16488 correction14 12-07-2012-E 24-Lead ML-24-6) ADIS16488AMLZ ML-24-6 D10277-0-4/14	PDF
Contextual Info: 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	Original	UG-287 32-bit 64-bit ADIS16xxx 16-pin UG09902-0-2/13	PDF

Contextual Info: Tactical Grade Ten Degrees of Freedom Inertial Sensor ADIS16488A Data Sheet FEATURES GENERAL DESCRIPTION Triaxial, digital gyroscope, ±450°/sec dynamic range <±0.05° orthogonal alignment error 5.1°/hr in-run bias stability 0.26°/√hr angular random walk	Original	ADIS16488A correc12-07-2012-E 24-Lead ML-24-6) ADIS16488BMLZ ADIS16488CMLZ ML-24-6	PDF