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SI‑MINS200S MEMS INS | Lightweight ≤0.6kg, High-Reliability for Unmanned Vehicle Navigation

SI‑MINS200S MEMS INS | Lightweight ≤0.6kg, High-Reliability for Unmanned Vehicle Navigation

MOQ: 1set
Delivery Period: 6-8 weeks
Payment Method: L/C,D/A,D/P,T/T,Western Union
Detail Information
Brand Name
SI
Model Number
SI-MINS200S
Technology:
Micro-Electro-Mechanical Systems (MEMS)
Size:
Compact And Lightweight
Function:
Inertial Navigation And Positioning
Interface:
4 Serial Ports (RS232 Or RS422) Support PPS
Accuracy:
High Precision
Productname:
MEMS Inertial Navigation System
Applications:
Drones, Robotics, Automotive Navigation, Wearable Devices
Highlight:

MEMS INS lightweight navigation system

,

high-reliability MEMS inertial navigation

,

unmanned vehicle navigation INS

Product Description

This new‑generation MEMS inertial/satellite integrated navigation system integrates a high‑precision survey‑grade satellite receiver board, three‑axis MEMS gyroscopes, and three‑axis MEMS accelerometers. It delivers centimeter‑level positioning accuracy under favorable satellite signal conditions and sustains long-term stable output of precise position, velocity and attitude data.

Featuring a lightweight, compact and easy‑to‑integrate design, the system is widely applicable to assisted driving, autonomous vehicles, vehicle positioning and orientation, AGV robots, power line inspection, platform stabilization, surveying and mapping, and precision agriculture scenarios.

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 MEMS INS | Lightweight ≤0.6kg, High-Reliability for Unmanned Vehicle Navigation
Products
PRODUCTS DETAILS
SI‑MINS200S MEMS INS | Lightweight ≤0.6kg, High-Reliability for Unmanned Vehicle Navigation
MOQ: 1set
Delivery Period: 6-8 weeks
Payment Method: L/C,D/A,D/P,T/T,Western Union
Detail Information
Brand Name
SI
Model Number
SI-MINS200S
Technology:
Micro-Electro-Mechanical Systems (MEMS)
Size:
Compact And Lightweight
Function:
Inertial Navigation And Positioning
Interface:
4 Serial Ports (RS232 Or RS422) Support PPS
Accuracy:
High Precision
Productname:
MEMS Inertial Navigation System
Applications:
Drones, Robotics, Automotive Navigation, Wearable Devices
Minimum Order Quantity:
1set
Delivery Time:
6-8 weeks
Payment Terms:
L/C,D/A,D/P,T/T,Western Union
Highlight

MEMS INS lightweight navigation system

,

high-reliability MEMS inertial navigation

,

unmanned vehicle navigation INS

Product Description

This new‑generation MEMS inertial/satellite integrated navigation system integrates a high‑precision survey‑grade satellite receiver board, three‑axis MEMS gyroscopes, and three‑axis MEMS accelerometers. It delivers centimeter‑level positioning accuracy under favorable satellite signal conditions and sustains long-term stable output of precise position, velocity and attitude data.

Featuring a lightweight, compact and easy‑to‑integrate design, the system is widely applicable to assisted driving, autonomous vehicles, vehicle positioning and orientation, AGV robots, power line inspection, platform stabilization, surveying and mapping, and precision agriculture scenarios.

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 MEMS INS | Lightweight ≤0.6kg, High-Reliability for Unmanned Vehicle Navigation