Inertial Measurement Unit ADIS16488 Small Size And High Overload Resistance IMU
Low Bias Stability IMU 16488 High Precision MEMS Inertial Devices With Built In GPS / BD Dual Mode Satellite R
IMU16488B is a domestic inertial measurement unit with high performance, small size and high overload resistance.
The gyro bias stability is 1.2 °/H (Allan) and the accelerometer bias stability is 50 µg (Allan). It can be used for precise
navigation, control and dynamic measurement of weapons. This series of products adopt high-precision MEMS inertial
devices, which have high reliability and high robustness, and can accurately measure the angular velocity and
acceleration information of moving carriers in harsh environments.
Product features:
※ High Precision MEMS Inertial Navigation ※ GPS/BD Dual Mode
※ Integrated navigation, AHRS, vertical gyro and other working modes
※ Support dynamic fast alignment ※ High bandwidth, 400Hz data update rate
※ External interface: 1-channel SPI and 1-channel UART
※ Support multiple external sensor combinations (odometer/DVL)
※ Small size, light weight ※ Strong and reliable
※ Fully compatible with a foreign 10-Dof inertial measurement system
Main technical indicators
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Test conditions |
Minimum value |
Typical value |
Maximum value |
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Measuring range |
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| Zero bias stability | Allan variance |
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deg /h | |
| Random walk |
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deg /√h | ||
| Zero-bias repeatability |
−40°C ≤ TA ≤ +85°C |
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| Scale factor repeatability |
Full temperature range −40°C ≤ TA ≤ +85°C |
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| Scale factor nonlinearity | FS=450 º/s |
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±5 |
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| Zero bias stability |
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| Random walk |
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| Zero-bias repeatability |
Full temperature range −40°C ≤ TA ≤ +85°C |
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| Scale factor repeatability |
Full temperature range −40°C ≤ TA ≤ +85°C |
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| Scale factor nonlinearity |
0.1 |
0.2 |
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Hz 3dB | ||||
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Dynamic measuring range |
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| Noise density |
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Pressure range |
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| Absolute measurement accuracy |
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Externally based Inertial satellite Integrated navigation |
Heading accuracy | Single GNSS, Maneuver Required, RMS |
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| Pitch and roll accuracy | GNSS Valid, RMS |
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| GNSS invalid, unlimited time, RMS |
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| Position accuracy | GNSS Valid, Single Point L1/L2, RMS |
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| Speed accuracy | GNSS Valid, Single Point L1/L2, RMS |
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| Communication interface | 1-way SPI | Baud rate |
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| 1-way UART | Baud rate |
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| Electrical characteristics |
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| Power consumption |
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| Structural characteristics |
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| Use environment | Operating temperature |
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| Storage temperature |
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(Half-sine 0.5msec) |
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| Continuous working time |
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IMU polarity definition
3 gyros and 3 accelerometers is defined as shown in the figure below, and the direction of the arrow is positive.
