Lightweight MEMS IMU for UAV Flight Control and Stabilization

Brand Name:Firepower
Model Number:16488D
Minimum Order Quantity:1
Delivery Time:10 days for sample
Payment Terms:T/T,L/C
Place of Origin:CHINA
Contact Now

Add to Cart

Verified Supplier
Location: Shenzhen Guangdong China
Address: 429, Building A10, Fuhai Information Port, Xinhe Community, Fuhai Street, Shenzhen, Guangdong, China
Supplier`s last login times: within 22 hours
Product Details Company Profile
Product Details

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

0.13

º/√h

Zero-bias repeatability

5

º/h

Output noise

No filtering, RMS

0.02

º/s

Scale factor nonlinearity

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

0.015

m/s/√h

Zero-bias repeatability

1

mg

Output noise

No filtering, RMS

0.2

mg

Scale factor

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

3.Outline and structure

Lightweight MEMS IMU for UAV Flight Control and Stabilization

China Lightweight MEMS IMU for UAV Flight Control and Stabilization supplier

Lightweight MEMS IMU for UAV Flight Control and Stabilization

Inquiry Cart 0