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SI‑MINS200S Compact & High‑Reliability MEMS INS, Weight ≤ 0.6 kg for UAV, UGV & USV Integrated Navigation
SI‑MINS200S Compact & High‑Reliability MEMS INS, Weight ≤ 0.6 kg for UAV, UGV & USV Integrated Navigation
Specifications
MOQ :
1set
Technology :
Micro-Electro-Mechanical Systems (MEMS)
Model Number :
SI-MINS200S
Size :
Compact and lightweight
Delivery Time :
6-8 weeks
Productname :
MEMS Inertial Navigation System
Accuracy :
High precision
Applications :
Drones, robotics, automotive navigation, wearable devices
Interface :
4 serial ports (RS232 or RS422) Support PPS
Function :
Inertial navigation and positioning
Brand Name :
SI
Payment Terms :
L/C,D/A,D/P,T/T,Western Union
Description

This product is a new generation of micro-electromechanical inertial/satellite combined navigation system, consisting of a high-precision survey-grade satellite receiver board, three-axis MEMS gyroscopes, and three-axis MEMS accelerometer.

It can provide centimeter-level positioning accuracy in environments with good satellite conditions and maintain precise location, speed, and attitude over extended periods.

The product is designed to be lightweight, compact, and user-friendly. It is suitable for various applications such as assisted driving, autonomous vehicles, vehicle positioning and orientation, AGV cars, power line inspection, platform stabilization, surveying and mapping, precision agriculture, and more.

Main technical parameters

System Real-time Accuracy
Heading 0.1° (single antenna, with good GNSS/DB signal); 0.1° (dual antennas, baseline ≥2m)
Attitude 0.05° (1σ, with good GNSS/DB signal); RTK: 0.1 (1σ).
Position 2m (CEP) (single antenna, with good GNSS/DB signal); RTK ≤2cm + 1ppm (CEP) (with good GNSS/DB signal)
Speed Accuracy 0.05m/s (1σ, with good GNSS/DB signal)
Rate of data update 200Hz(max)
Startup time ≤10s
Post-processing Accuracy
Heading 0.05°(1σ)
Attitude 0.03°(1σ)
Position Accuracy 2cm+1ppm(CEP)
Main Device Characteristics
Gyroscope range ±500°/s Zero Bias Stability
≤5°/h(10s smoothing, 1σ)
Accelerometer range ±10g Zero Bias Stability
≤20μg (10s smoothing, 1σ)
Physical Characteristic Interface 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 Rate 9600～961200bps(configurable)
Protection level IP65 User 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

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Product Detail
MOQ :
1set
Technology :
Micro-Electro-Mechanical Systems (MEMS)
Model Number :
SI-MINS200S
Size :
Compact and lightweight
Delivery Time :
6-8 weeks
Productname :
MEMS Inertial Navigation System
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
Main Products :
MEMS Inertial Measurement Unit, MEMS Inertial Navigation System, Single Axis Gyroscope
Total Annual :
5000000-10000000
Employee Number :
500~1000
Certification Level :
Verified Supplier
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