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Lightweight MEMS IMU for UAV Flight Control and Stabilization

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Lightweight MEMS IMU for UAV Flight Control and Stabilization

Name: Lightweight MEMS IMU for UAV Flight Control and Stabilization
Brand: Firepower
Price: 2000 USD

Wholesale Lightweight MEMS IMU for UAV Flight Control and Stabilization from china suppliers

Brand Name : Firepower

Model Number : 16488D

Place of Origin : CHINA

MOQ : 1

Payment Terms : T/T,L/C

Supply Ability : 1000/month

Delivery Time : 10 days for sample

Packaging Details : carton with sponge

Price : 2000$

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 : 1W

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Overview

The 16488D is a high-performance inertial measurement unit that is precisely calibrated over the full temperature range to meet performance requirements under varying conditions. Built-in three-axis gyroscope and three-axis accelerometer are used to measure the three-axis angular rate, acceleration and other parameters of the carrier, and output the data after error compensation (including temperature compensation, installation misalignment angle compensation, nonlinear compensation, etc.) through SPI according to the communication protocol.

Performance indicators

The specific performance index configuration of 16488D is shown in Table 1:

Table 1 Performance index

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 ℃, 10 s 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 ℃, 10 s 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
Magnetometer	Resolution			0.1		mg
Barometer	Range		260		1260	hPa
Barometer	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

3.Outline and structure

Lightweight MEMS IMU for UAV Flight Control and Stabilization

Product Tags:

10'' 3 Axis Turntable

Angular Position 3 Axis Turntable

Lightweight MEMS IMU for UAV Flight Control and Stabilization Images

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