Specifications
MOQ :
1set
Model Number :
SI-MINS200S
Delivery Time :
6-8 weeks
Interface :
4 serial ports (RS232 or RS422) Support PPS
Size :
Compact and lightweight
Applications :
Drones, robotics, automotive navigation, wearable devices
Technology :
Micro-Electro-Mechanical Systems (MEMS)
Function :
Inertial navigation and positioning
Productname :
MEMS Inertial Navigation System
Brand Name :
SI
Accuracy :
High precision
Payment Terms :
L/C,D/A,D/P,T/T,Western Union
Description

This integrated navigation system adopts a high-precision survey-grade satellite receiver board, paired with high-performance triaxial MEMS gyroscopes and triaxial MEMS accelerometers. As a compact MEMS-based GNSS/INS combined navigation unit, it supports single-antenna dynamic alignment and dual-antenna RTK high-precision rapid orientation.

Equipped with an upgraded integrated navigation algorithm engine and optimized SE anti-interference design, the product effectively resists satellite occlusion and multipath interference. It delivers long-term, high-precision and highly reliable navigation performance even in complex urban and canyon scenarios. Under favorable satellite conditions, it achieves centimeter-level positioning accuracy and provides stable, continuous output of position, velocity and attitude data for prolonged operation.

Featuring ultra-lightweight, compact structure and easy integration, this unit is widely applied in assisted driving, autonomous vehicles, vehicle positioning and orientation, AGV robots, power line inspection, platform stabilization, surveying and mapping, and precision agriculture.

Main technical parameters

System Real-time Accuracy
Heading0.1° (single antenna, with good GNSS/DB signal); 0.1° (dual antennas, baseline ≥2m)
Attitude0.05° (1σ, with good GNSS/DB signal); RTK: 0.1 (1σ).
Position2m (CEP) (single antenna, with good GNSS/DB signal); RTK ≤2cm + 1ppm (CEP) (with good GNSS/DB signal)
Speed Accuracy0.05m/s (1σ, with good GNSS/DB signal)
Rate of data update200Hz(max)
Startup time≤10s
Post-processing Accuracy
Heading0.05°(1σ)
Attitude0.03°(1σ)
Position Accuracy2cm+1ppm(CEP)
Main Device Characteristics
Gyroscoperange±500°/sZero Bias Stability
≤5°/h(10s smoothing, 1σ)

Accelerometerrange±10gZero Bias Stability
≤20μg (10s smoothing, 1σ)
Physical CharacteristicInterface Characteristics
Supply voltage
24V DC rated(12~32V DC)
Interface method

4 serial ports (RS232 or RS422)

Support PPS, EVENTMARK input/output

Power consumption
<8±0.5W
Operating temperature
-40℃~﹢55℃
Transmission Rate9600~961200bps(configurable)
Protection levelIP65User Mode
Physical dimension≤110mm×81mm×68mm


Vehicle-mounted (default), aircraft-mounted, ship-mounted

Weight≤0.6Kg

SI‑MINS200S Compact & High‑Reliability MEMS INS, Weight ≤ 0.6 kg for UAV, UGV & USV Integrated Navigation

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SI‑MINS200S Compact & High‑Reliability MEMS INS, Weight ≤ 0.6 kg for UAV, UGV & USV Integrated Navigation

Ask Latest Price
MOQ :
1set
Model Number :
SI-MINS200S
Delivery Time :
6-8 weeks
Interface :
4 serial ports (RS232 or RS422) Support PPS
Size :
Compact and lightweight
Applications :
Drones, robotics, automotive navigation, wearable devices
Contact Supplier
SI‑MINS200S Compact & High‑Reliability MEMS INS, Weight ≤ 0.6 kg for UAV, UGV & USV Integrated Navigation

Stable Inertial Systems Ltd.

Verified Supplier
1 Years
beijing, beijing
Since 1997
Business Type :
Manufacturer, Seller
Total Annual :
5000000-10000000
Employee Number :
500~1000
Certification Level :
Verified Supplier
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