MAH-A301
MEMS AHRS
Product Overview
The MAH-A301 is a high-reliability and cost-effective 6-axis attitude heading reference system. This module implements full-temperature compensation for bias, scale factor, non-orthogonality error and acceleration-related terms, sustaining stable and high measurement accuracy over long working hours.
It adopts integral vibration damping and hermetic sealing design. It can withstand severe vibration and shock conditions, widely applied in attitude measurement, control and measurement domains including satellite payloads, land vehicles, ships and UAVs.
Core Advantages
Full-temperature calibration compensation from -45℃ to +80℃, compact size, light weight and low power consumption. The built-in adaptive attitude heading algorithm ensures stable roll, pitch and yaw output. It supports 1kHz high-speed sampling and delivers consistent performance under harsh mechanical environments.
Key Features of This MEMS AHRS
- -45℃ ~ +80℃ full-temperature calibration & compensation
- Small size, light weight and low power consumption
- Adaptive attitude heading algorithm for stable output
- 1kHz high-speed sampling rate
- Robust structure resistant to harsh mechanical environments
Main Applications
- UAV attitude measurement & flight control
- Vehicle and marine attitude monitoring
- Satellite-borne motion sensing
- Platform stabilization systems
- Industrial dynamic attitude monitoring
Attitude Sensor vs INS Clarification
This MEMS AHRS outputs roll, pitch and yaw attitude data only, without position or velocity navigation solving. If you need a full inertial navigation system (INS) which calculates position and velocity, please check our FOG inertial navigation product.
You can learn more about the working principle of an attitude heading reference system from Advanced Navigation AHRS introduction.
Performance Specifications
| Category | Parameter Item | MAH-A301 |
|---|---|---|
| Gyroscope | Range (°/s) | ±300 |
| Full-temperature Bias (°/h, 3σ) | ≤ 0.1 | |
| Bias Stability (°/h, 10s smooth) | ≤ 0.1 | |
| Bias Stability (°/h, allan, typ) | ≤ 0.01 | |
| Bias Repeatability (°/h) | ≤ 0.05 | |
| Angular Random Walk (°/√h) | ≤ 0.005 | |
| Scale Factor Nonlinearity (ppm) | ≤ 150 | |
| Cross Coupling (rad) | ≤ 0.001 | |
| Bandwidth (Hz) | ≥ 100 | |
| Accelerometer | Range (g) | ±30 |
| Full-temperature Bias (mg) | ≤ 2 | |
| Bias Stability (μg, 10s smooth) | ≤ 100 | |
| Bias Repeatability (μg) | ≤ 100 | |
| Scale Factor Nonlinearity (ppm) | ≤ 500 | |
| Bandwidth (Hz) | ≥ 150 | |
| AHRS System | Pitch Measurement Range (°) | ±90 |
| Roll Measurement Range (°) | ±180 | |
| Attitude Accuracy (°, RMS) | Steady-state ≤0.1; Low dynamic ≤0.5 | |
| Electrical & Mechanical Interface | Power Supply (V) | 5-12 |
| Static Power Consumption (W) | ≤ 2 | |
| Start-up Time (s) | ≤ 2 | |
| Update Rate (Hz, max) | 200 | |
| Dimension (mm×mm×mm) | 47×47×28 | |
| Weight (g) | ≤ 200 | |
| Operating Temperature (℃) | -45 ~ +80 | |
| Operating Environment | Storage Temperature (℃) | -55 ~ +85 |
| Vibration (g, RMS) | 20~2000Hz, 6.06 | |
| Shock (g) | 1000g/1ms |