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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
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 |
| ±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 | ||||
|
| 30g,11ms | |||||
| Overload | (Half-sine 0.5msec) | 1000g | ||||
Dimensions

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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 Images |