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IP65 MEMS INS Inertial Navigation System Integrated Inertial Navigation Unit For Aircraft

IP65 MEMS INS Inertial Navigation System Integrated Inertial Navigation Unit For Aircraft

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
Productname:
MEMS Inertial Navigation System
Technologytype:
MEMS (Micro-Electro-Mechanical Systems)
Navigationtype:
Inertial Navigation
Protection Level:
IP65
Operating Temperature:
-40℃~﹢55℃
Supply Voltage:
24V DC Rated(12~32V DC)
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MEMS INS Inertial Navigation System

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MEMS Inertial Navigation Unit For Aircraft

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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 parameter

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

 

IP65 MEMS INS Inertial Navigation System Integrated Inertial Navigation Unit For Aircraft 0