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Lightweight MEMS IMU for UAV Flight Control and Stabilization

Name: Lightweight MEMS IMU for UAV Flight Control and Stabilization
Brand: Shenzhen Fire Power Control Technology Co., LTD
SKU: 16488D
Price: 2000 USD
Availability: InStock

Brand Name:	Firepower
Model Number:	16488D
MOQ:	1
Price:	2000$
Payment Terms:	T/T,L/C
Supply Ability:	1000/month

Detail Information

Product Description

Detail Information

Place of Origin:

CHINA

Gyroscope Range:

±500º/s

Zero-bias Instability:

1º/h

Zero Bias Stability:

7º/h

Random Walk:

0.13 º/√h

Accelerometer Measuring Range:

18ug

Zero-bias Repeatability:

1mg

Bandwidth:

280 Hz

Power Consumption:

Packaging Details:

carton with sponge

Supply Ability:

1000/month

Highlight:

10'' 3 Axis Turntable

Angular Position 3 Axis Turntable

Product Description

Lightweight MEMS IMU for UAV Flight Control and Stabilization

Overview

The 16488D is a high-performance inertial measurement unit precisely calibrated over the full temperature range to maintain performance under varying conditions. It features a built-in three-axis gyroscope and three-axis accelerometer to measure angular rate, acceleration, and other parameters. The unit outputs error-compensated data (including temperature compensation, installation misalignment angle compensation, and nonlinear compensation) via SPI communication protocol.

Performance Indicators

The 16488D's performance specifications are detailed in the following table:

Parameter	Test Conditions	Minimum Value	Typical Value	Maximum Value	Unit
Gyroscope
Dynamic measuring range				±500	º/s
Zero-bias instability	Allan variance		1		º/h
Zero bias stability	1s smooth, RMS		7		º/h
Zero bias in full temperature range	-40℃ ~ 85℃, 10s smoothing, RMS		0.007		º/s
Random walk	1σ		0.13		º/√h
Zero-bias repeatability	1σ		5		º/h
Output noise	No filtering, RMS		0.02		º/s
Scale factor nonlinearity	1σ		0.01		%
Scale factor	FS=500 º/s		524.287		LSB/°/sec
Bandwidth (-3dB)			150	280	Hz
Cross coupling			0.05		%
Acceleration sensitivity			10.7		°/h/g
Resonant frequency			19k		Hz
Accelerometer
Dynamic measuring range				±16	g
Zero bias stability	Allan variance		18		ug
Zero bias in full temperature range	-40℃ ~ 85℃, 10s smoothing, RMS		0.3		mg
Random walk	1σ		0.015		m/s/√h
Zero-bias repeatability	1σ		1		mg
Output noise	No filtering, RMS		0.2		mg
Scale factor	1σ		16383		g/LSB
Bandwidth (-3dB)			150	280	Hz
Cross coupling			0.05		%
Magnetometer
Range				2(8)	guass
Resolution			0.1		mg
Barometer
Range		260		1260	hPa
Resolution			4096		LSB/hPa
Temperature
Scale factor			0.019		°C/LSB
Communication Interface
1-way SPI	Enter the clock frequency		6	12	MHz
Electrical Characteristics
Voltage	Direct current	3	3.3	3.6	V
Power consumption			1		W
Ripple	P-P		50		mV
Use Environment
Operating temperature	Scalable	-40		85	℃
Storage temperature		-55		105	℃
Impact			2000g

Outline and Structure

Tags:

Accelerometer Gyro Sensor

IMU Accelerometer Gyro

Quartz Flexure Accelerometer

Fiber Optic Gyro

Inertial Navigation System

Gyro North Finder

Magnetometer Sensor

Accelerometer Gyro Sensor

IMU Accelerometer Gyro

Quartz Flexure Accelerometer

Fiber Optic Gyro

Inertial Navigation System

Gyro North Finder

Magnetometer Sensor

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Lightweight MEMS IMU for UAV Flight Control and Stabilization

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