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Inertial Navigation

SDI-MAHRS

The Micro Heading Attitude Reference System (SDI-MAHRS) series is a miniature full-attitude measurement sensor device, which consists of three types of sensors, including a three-axis MEMS gyroscope, a three-axis MEMS accelerometer, and a three-axis magnetoresistive magnetometer. constitute. The three-axis gyroscope is used to measure the absolute angular rate of the carrier in three directions, and the three-axis accelerometer is used to measure the acceleration of the carrier in three directions. For the drift in the pitch and roll directions, the three-axis magnetoresistive magnetometer measures the three-dimensional geomagnetic intensity, which is used to provide the initial alignment of the orientation angle and correct the drift of the heading angle. Micro attitude reference system INS-MAHRS series, the output data that can be provided are: raw data, quaternion, attitude data, etc.

Features

  • High performance&Low price
  • Sealed design&Dynamic measurement
  • RS-232 serial interface for easy connection
  • Real-time triaxial inertial output

Application

  • Autonomous navigation
  • Automatic control
  • Attitude measurement

Physical and electrical

Voltage 4.5~9VDC
Power ≤1W
Weight ≤20g
Dimensions 76mm×76mm×22.5mm

Performance

Output data format Raw data/Attitude angle/Quaternion
Update rate 100Hz
Start time 1s
Heading accuracy ±0.5°(Static)
±1° (Dynamic)
Pitch/Roll accuracy ±0.1°(Static)
±0.5°(Dynamic)
Heading angle resolution 0.1°
Gyro Range: ±2000°/s
Zero Bias Stability: ±0.2°/s
Non-linea: 0.2 %
Accelerometer Range: ±8g
Zero Bias Stability: ±0.003g
Non-linear: 0.2 %
Magnetometer Range: ±1.3 Gauss
Zero Bias Stability: 0.01° Gauss
Non-linear: 0.4 %

Environmental

Operating -40℃~67℃
Storage -55℃~70℃