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GS16488 Inertial Measurement Unit with 1 Channel SPI, Bias Repeatability −40°C ≤ TA ≤ +85°C, and Scale Factor Nonlinearity FS=450 º/s

Categories Accelerometer Sensor
Brand Name: Gyrosens
Model Number: GS16488
Certification: CE
Place of Origin: china
MOQ: 1pcs
Payment Terms: D/A,L/C,D/P,T/T,Western Union,MoneyGram
Supply Ability: 1000 Piece/Pieces per Week negotiable
Delivery Time: 5-8 work days
Packaging Details: each unit has individual box and all boxes are packed in standard packages or customers requests available
Bias Repeatability: −40°C ≤ TA ≤ +85°C
Scale factor nonlinearity: FS=450 º/s
Scale factor repeatability: −40°C ≤ TA ≤ +85°C
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GS16488 Inertial Measurement Unit with 1 Channel SPI, Bias Repeatability −40°C ≤ TA ≤ +85°C, and Scale Factor Nonlinearity FS=450 º/s

Product Introduction

Inertial measurement Unit GS16488 is a domestic inertial measurement equipment with high performance, small size and high overload resistance. Gyroscope zero bias stability 0.5°/h (Allan), accelerometer zero bias stability 10µg (Allan). It can be used for precise navigation, control and dynamic measurement of weapons. This series of products adopts high-precision MEMS inertial devices, with high reliability and high robustness, and can accurately measure the angular velocity and acceleration information of the moving carrier in harsh environments.

The inertial measurement unit GS16488 with built-in three-axis gyro and three-axis accelerometer is used to measure the carrier's three-axis angular rate and three-axis acceleration. Through the serial port according to the convention communication protocol output error compensation (including temperature compensation, installation misalignment Angle compensation, nonlinear compensation, etc.) gyroscope, accelerometer data, and built-in three-axis magnetic sensor, pressure sensor.

Key Features

High precision MEMS inertial navigation

Support dynamic fast alignment

High bandwidth, high data update rate

1 channel SPI

Small size, light weight

Solid and reliable

Fully compatible with a foreign 10 °rees of freedom inertial measurement system

Application

Unmanned aerial vehicle

Aerial photography

Agricultural plant protection

The photoelectric detection is stable

In-vehicle navigation

Vehicle satellite communication

Forest and land monitoring

High-speed railway track inspection

Technical Specifications

Parameter

Test condition

MIN

TYP

MAX

Uints

Power supply parameter

Voltage

3.0

3.3

3.6

V

Power dissipation

1.5

W

Ripple

P-P

100

mV

Product performance

Gyroscope

Range

±400

±450

°/s

Bias stability

Allan

0.8

° /h

Random walk

0.06

° /√h

Bias Repeatability

40°C ≤ TA ≤ +85°C

0.1

0.2

°/s

Scale factor repeatability

40°C ≤ TA ≤ +85°C

0.1

1

%

Scale factor nonlinearity

FS=450 º/s

0.1

0.2

%FS

Bandwidth

400

Hz

Accelerometer

Range

±10

g

Bias stability

Allan

0.01

mg

Random walk

0.02

0.02

m/s/√h

Bias Repeatability

40°C ≤ TA ≤ +85°C

±2

mg

Scale factor repeatability

40°C ≤ TA ≤ +85°C

0.5

1

%

Scale factor nonlinearity

0.1

%FS

Bandwidth

200

Hz

Magnetometer

Dynamic measuring range

±2.5

gauss

Resolution

120

uGauss

Noise density

50

uGauss

Bandwidth

200

Hz

Barometer

Pressure range

450

1100

mbar

Resolution

0.1

mbar

Absolute measurement accuracy

1.5

mbar

Communication interface

One SPI

Baud rate

15

MHz

Structural characteristics

Size

44×47×14

mm

Size

Weight

50

g

Weight

Reliability

MTBF

20000

h

Continuous working hours

120

h

Environment

Operating temperature

-40

75

°C

Storage temperature

-45

85

°C

Vibration

10~2000Hz,3g

Impact

30g,11ms

Overload

(Half-sine 0.5msec)

1000g


Dimensions

Quality GS16488 Inertial Measurement Unit with 1 Channel SPI, Bias Repeatability −40°C ≤ TA ≤ +85°C, and Scale Factor Nonlinearity FS=450 º/s for sale
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