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IMU Accelerometer Gyro

Small Size Inertial Measurement Unit ADIS16488 And High Overload Resistance

Name: Small Size Inertial Measurement Unit ADIS16488 And High Overload Resistance
Brand: Shenzhen Fire Power Control Technology Co., LTD
SKU: 16480G
Price: 3,003.00 USD
Availability: InStock

Brand Name:	Firepower
Model Number:	16480G
MOQ:	1
Price:	negotiable
Payment Terms:	T/T,L/C
Supply Ability:	500/month

Detail Information

Product Description

Detail Information

Place of Origin:

CHINA

Certification:

CE ROHS

Product Name:

MEMS Inertial Measurement Unit

Measuring Range:

±450º/s

Zero Bias Stability:

2deg/h

Random Walk:

0.1deg /√h

Zero-bias Repeatability:

0.1deg/s

Bandwidth:

400Hz

Packaging Details:

sponge/box

Supply Ability:

500/month

Highlight:

Small Inertial Measurement Unit

ADIS16488 Inertial Measurement Unit

2deg/h IMU Accelerometer Gyro

Product Description

Inertial Measurement Unit ADIS16488 Small Size And High Overload Resistance IMU

IMU16488B is a domestic inertial measurement unit with high performance, small size and high overload resistance.

The gyro bias stability is 1.2 °/H (Allan) and the accelerometer bias stability is 50 µg (Allan). This series of products adopt high-precision MEMS inertial

devices, which have high reliability and high robustness, and can accurately measure the angular velocity and acceleration information of moving carriers in harsh environments.

Main technical indicators

		Test conditions	Typical value	Maximum value
	Measuring range
	Zero bias stability	Allan variance			deg /h
	Random walk				deg /√h
	Zero-bias repeatability	−40°C ≤ TA ≤ +85°C
	Scale factor repeatability	Full temperature range −40°C ≤ TA ≤ +85°C
	Scale factor nonlinearity	FS=450 º/s

			±5
	Zero bias stability
	Random walk
	Zero-bias repeatability	Full temperature range −40°C ≤ TA ≤ +85°C
	Scale factor repeatability	Full temperature range −40°C ≤ TA ≤ +85°C
	Scale factor nonlinearity		0.1	0.2
					Hz 3dB
	Dynamic measuring range

	Noise density

	Pressure range

	Absolute measurement accuracy
Externally based Inertial satellite Integrated navigation	Heading accuracy	Single GNSS, Maneuver Required, RMS
	Pitch and roll accuracy	GNSS Valid, RMS
	Pitch and roll accuracy	GNSS invalid, unlimited time, RMS
	Position accuracy	GNSS Valid, Single Point L1/L2, RMS
	Speed accuracy	GNSS Valid, Single Point L1/L2, RMS
Communication interface	1-way SPI	Baud rate
Communication interface	1-way UART	Baud rate
Electrical characteristics
	Power consumption

Structural characteristics
Structural characteristics
Use environment	Operating temperature
	Storage temperature
			,3g
			,11ms
		(Half-sine 0.5msec)

	Continuous working time

IMU polarity definition

3 gyros and 3 accelerometers is defined as shown in the figure below, and the direction of the arrow is positive.

Tags:

Accelerometer Gyro Sensor

IMU Accelerometer Gyro

Quartz Flexure Accelerometer

Fiber Optic Gyro

Inertial Navigation System

3 Axis Turntable

Gyro North Finder

Accelerometer Test Equipment

Magnetometer Sensor

1 Axis Turntable

2 Axis Turntable

Accelerometer Gyro Sensor

IMU Accelerometer Gyro

Quartz Flexure Accelerometer

Fiber Optic Gyro

Inertial Navigation System

3 Axis Turntable

Gyro North Finder

Accelerometer Test Equipment

Magnetometer Sensor

1 Axis Turntable

2 Axis Turntable

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Small Size Inertial Measurement Unit ADIS16488 And High Overload Resistance

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