Product - MEMS INS

MEMS INS/GNSS Integrated System

It integrates a MEMS Inertial Measurement Unit (IMU) and a Global Navigation Satellite System (GNSS) receiver, with a built-in navigation algorithm that directly outputs position, velocity, and attitude data. The dual-inertial design (Inertial + GNSS) ensures stable navigation even in GNSS-denied environments.

MS20062

Gyroscope Bias Stability (10s Smoothed): ≤10°/h (XY Axis), ≤5°/h (Z Axis)
Accelerometer Bias Stability: ≤100μg (10s Smoothed)
System-Level Accuracy: Combined Heading 0.15° (Dual Antenna), Position 3m (Single Point)

MS60081

Gyroscope Bias Stability (10s Smoothed): 0.3°/h
Accelerometer Bias Stability: ≤20μg
System-Level Accuracy: Self-North-Seeking ≤1×sec(L) (L=Latitude), Heading ≤0.1° (Dual Antenna)

MS6008

Gyroscope Bias Stability (10s Smoothed): 0.1°/h
Accelerometer Bias Stability: ≤20μg
System-Level Accuracy: Self-North-Seeking ≤0.5×sec(L) (L=Latitude), Heading ≤0.1° (Dual Antenna)

MEMS Positioning and Orientation System

Centered on high-precision attitude measurement, integrated with self-alignment (north-finding) function, and compatible with external odometers for accurate dead reckoning.

MS8000

Gyroscope Bias Stability (10s Smoothing): ＜0.1°/h
Accelerometer Bias Stability: ＜0.05mg
System-Level Accuracy: Self-Aligning North ≤3mil, Attitude ≤0.5mil
Industry Positioning: Benchmark for High-Precision Automotive Applications

MEMS Inertial Measurement Unit (MEMS IMU)

Outputs raw data from 3-axis gyroscope (angular rate) + 3-axis accelerometer (linear acceleration). No built-in navigation solution; requires external algorithms for navigation processing.

MU2018

Gyroscope Bias Stability (10s Smoothing): ≤15°/h
Accelerometer Bias Stability: ≤300μg
Industry Positioning: Mid-Range Industrial Grade

MU4000 Series

Gyroscope Bias Stability (10s Smoothing): 0.3°/h ~ 3°/h
Accelerometer Bias Stability: ≤80μg
Industry Positioning: Industrial Grade

MU6000 Series

Gyroscope Bias Stability (10s Smoothing): 0.1°/h ~ ≤3°/h
Accelerometer Bias Stability: ≤10μg (Allan)
Industry Positioning: Tactical Grade

MU8008

Gyroscope Bias Stability (10s Smoothing): ≤0.5°/h (Optional: ≤0.3°/h)
Accelerometer Bias Stability: ≤30μg (Allan)
Industry Positioning: Tactical Grade Alternative

MEMS Attitude and Heading Reference System (AHRS) / North Finder

Integrates IMU and attitude/heading calculation algorithms, outputs pitch, roll, and heading data. Some models support north-finding.

MU4016

Gyroscope Bias Stability (10s Smoothing): ≤0.3°/h
Accelerometer Bias Stability: ≤100μg
System-Level Accuracy: Attitude ≤0.1° (Static State), ≤0.5° (Low Dynamic State)
Industry Positioning: High-End Industrial Grade AHRS

MU4022

Gyroscope Bias Stability (10s Smoothing): ≤5°/h
Accelerometer Bias Stability: ≤100μg
System-Level Accuracy: Attitude ≤0.2° (Static State), ≤2° (Dynamic State)
Industry Positioning: Mid-Range Industrial Grade AHRS

MU6006

Gyroscope Bias Stability (10s Smoothing): 0.1°/h
Accelerometer Bias Stability: ≤100μg
System-Level Accuracy: North Seeking ≤0.5*sec (L), Heading Hold ≤0.5°/h
Industry Positioning: Tactical Grade North Seeker

Scene Matching Navigation Module

Based on visual map matching technology, it outputs position information and can be externally connected with an IMU to enhance navigation robustness. It serves as a supplementary solution for visual navigation.

VMN-S160

Split-Type Scene Matching Module
System-Level Accuracy: Positioning ≤40m (at 300m Altitude), ≤5% of Flight Altitude (300-3000m)
Industry Positioning: Visual Navigation Supplement

VMN-A160

Integrated Scene Matching Module
System-Level Accuracy: Positioning ≤40m (at 300m Altitude), ≤5% of Flight Altitude (300-3000m)
Industry Positioning: All-Time Visual Navigation