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Compact & High Reliability MEMS INS SI-MINS160S, Weight ≤0.6Kg for UAV, UGV & USV Integrated Navigation

Compact & High Reliability MEMS INS SI-MINS160S, Weight ≤0.6Kg for UAV, UGV & USV Integrated 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-MINS160S
Product Name:
MEMS Inertial Navigation System
Pitch And Roll:
≤0.05° (1σ)
Navigationtype:
Inertial Navigation
Heading:
≤0.15° (1σ)
Operating Temperature:
-40℃~﹢55℃
Supply Voltage:
24V DC Rated(12~32V DC)
Bias Stability:
≤10°/h
Highlight:

MEMS INS Inertial Navigation System

,

MEMS Inertial Navigation Unit For Aircraft

,

IP65 Integrated Inertial Navigation Unit

Product 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 0.15° (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 0.02°(1σ)
Position Accuracy 2cm+1ppm(CEP)
Main Device Characteristics
Gyroscope range ±500°/s Zero Bias Stability ≤10°/h(10s smoothing, 1σ)
Accelerometer range ±10g Zero Bias Stability ≤500μg (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
Compact & High Reliability MEMS INS SI-MINS160S, Weight ≤0.6Kg for UAV, UGV & USV Integrated Navigation
Products
PRODUCTS DETAILS
Compact & High Reliability MEMS INS SI-MINS160S, Weight ≤0.6Kg for UAV, UGV & USV Integrated 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-MINS160S
Product Name:
MEMS Inertial Navigation System
Pitch And Roll:
≤0.05° (1σ)
Navigationtype:
Inertial Navigation
Heading:
≤0.15° (1σ)
Operating Temperature:
-40℃~﹢55℃
Supply Voltage:
24V DC Rated(12~32V DC)
Bias Stability:
≤10°/h
Minimum Order Quantity:
1set
Delivery Time:
6-8 weeks
Payment Terms:
L/C,D/A,D/P,T/T,Western Union
Highlight

MEMS INS Inertial Navigation System

,

MEMS Inertial Navigation Unit For Aircraft

,

IP65 Integrated Inertial Navigation Unit

Product 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 0.15° (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 0.02°(1σ)
Position Accuracy 2cm+1ppm(CEP)
Main Device Characteristics
Gyroscope range ±500°/s Zero Bias Stability ≤10°/h(10s smoothing, 1σ)
Accelerometer range ±10g Zero Bias Stability ≤500μg (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
Compact & High Reliability MEMS INS SI-MINS160S, Weight ≤0.6Kg for UAV, UGV & USV Integrated Navigation