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9-Axis MEMS IMU 0.3°/h Gyro Bias for Drone Flight Control & GNSS-Denied Navigation

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9-Axis MEMS IMU 0.3°/h Gyro Bias for Drone Flight Control & GNSS-Denied Navigation

Name: 9Axis MEMS IMU 03h Gyro Bias for Drone Flight Control amp GNSSDenied Navigation
Brand: Firepower
Price: 1 USD

9-Axis MEMS IMU 0.3°/h Gyro Bias for Drone Flight Control & GNSS-Denied Navigation Manufactures

Brand Name : Firepower

Model Number : 16488HA

Certification : Military standard

Place of Origin : China

MOQ : 1

Price : negotiable

Payment Terms : T/T

Supply Ability : 50/month

Delivery Time : 20 days for sample

Packaging Details : sponge+ box

Random Walk : 0.15°/√h

Zero-bias instability : 0.3º/h

Zero Bias Repatability : ≤5°/h

Bandwidth : 250Hz

Scale Factor Nonlinear : ≤100ppm

Scale factor repeatability : ≤100ppm

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ADIS16488HA is a compact, lightweight MEMS IMU with three-axis gyroscope and accelerometer, measuring ±450°/s angular rate and ±20 g acceleration. Zero-bias instability is 0.3°/h for the gyro and 0.25 mg for the accelerometer, with minimal random walk and 100–500 ppm scale factor linearity. Temperature, misalignment, and nonlinear error compensation ensure reliable performance from -45~85 °C. SPI communication at 8–15 MHz, 1.5 W power consumption, 250 Hz bandwidth, and 0.1 % cross-coupling make it ideal for UAVs, robotics, industrial automation, mobile mapping, and precision navigaion systems.

Technical Parameters

Parameter		Test conditions	Minimum value	Typical value	Maximum value	Unit
Gyroscope	Dynamic measuring range			±450		º/s
	Zero-bias instability	Allan variance, better than		0.3		º/h
	Zero bias stability	10s smooth, RMS, better than		3		º/h
	Zero bias in full temperature range	-40 ℃ ~ 85 ℃, 10 s smooth, rms		20		º/h
	Random walk	1σ		0.15		º/√h
	Zero-bias repeatability	1σ		5		º/h
	Scale factor repeatability	1σ		100		ppm
	Scale factor nonlinearity	1σ		100		ppm
	Bandwidth (-3dB)			250		Hz
	Cross coupling			0.1		%
	Resolution			2		º/h
	Acceleration sensitivity			2		°/h/g
Accelerometer	Dynamic measuring range			±20		g
	Zero bias stability	Allan variance		0.07		mg

	Zero bias in full temperature range	-40 ℃ ~ 85 ℃, 10 s smooth, rms		3		mg
	Zero bias stability	10s smooth, RMS, better than		0.25		mg
	Random walk	1σ		0.029		m/s/√h
	Zero-bias repeatability	1σ		0.5		mg
	Scale factor repeatability	1σ		500		ppm
	Scale factor nonlinearity	FS=20g		500		ppm
	Bandwidth (-3dB)			250		Hz
	Cross coupling			0.1		%
Communication Interface	1-way SPI	Enter the clock frequency		8	15	MHz
Electrical characteristics	Voltage	Direct current		3.3		V
	Power consumption			1.5	1.5	W
	Ripple	P-P		48±2	100	mV
Use environment	Operating temperature		-45		85	℃
Use environment	Storage temperature		-55		85	℃

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9-Axis MEMS IMU 0.3°/h Gyro Bias for Drone Flight Control & GNSS-Denied Navigation

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axial direction

Product Tags:

high precision fiber optic gyro

100ppm fiber optic gyro

9-Axis MEMS IMU 0.3°/h Gyro Bias for Drone Flight Control & GNSS-Denied Navigation Images

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