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SI‑MINS160S MEMS INS | Compact ≤0.6kg for UAV UGV USV Integrated Navigation

SI‑MINS160S MEMS INS | Compact ≤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:

compact MEMS INS for UAV

,

lightweight MEMS inertial navigation system

,

integrated navigation system for UGV

Product Description

This product is a new‑generation MEMS inertial/satellite integrated navigation system. It incorporates 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 outputs stable precise position, velocity and attitude data for prolonged operation.

Featuring lightweight, compact and easy‑to‑integrate characteristics, the unit is widely applied in assisted driving, autonomous vehicles, vehicle positioning and orientation, AGV robots, power line inspection, platform stabilization, surveying and mapping, precision agriculture and other scenarios.

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

SI‑MINS160S MEMS INS | Compact ≤0.6kg for UAV UGV USV Integrated Navigation

Products
PRODUCTS DETAILS
SI‑MINS160S MEMS INS | Compact ≤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

compact MEMS INS for UAV

,

lightweight MEMS inertial navigation system

,

integrated navigation system for UGV

Product Description

This product is a new‑generation MEMS inertial/satellite integrated navigation system. It incorporates 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 outputs stable precise position, velocity and attitude data for prolonged operation.

Featuring lightweight, compact and easy‑to‑integrate characteristics, the unit is widely applied in assisted driving, autonomous vehicles, vehicle positioning and orientation, AGV robots, power line inspection, platform stabilization, surveying and mapping, precision agriculture and other scenarios.

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

SI‑MINS160S MEMS INS | Compact ≤0.6kg for UAV UGV USV Integrated Navigation