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| Categories | Fiber Optic Inertial Navigation System |
|---|---|
| Brand Name: | SI |
| Model Number: | SI-FINS60S |
| MOQ: | 1set |
| Payment Terms: | D/A,L/C,D/P,T/T,Western Union |
| Delivery Time: | 6-8 weeks |
| Bias Stability: | ≤0.08°/h |
| Pitch and roll: | ≤0.01° (1σ) |
| Applications: | Aerospace, marine navigation, autonomous vehicles, military |
| Navigation Type: | Inertial Navigation |
| Heading: | ≤0.04° (1σ) |
| Physical Dimensions: | ≤140mm×125mm×126mm |
| User Mode: | Vehicle-mounted (default), aircraft-mounted, ship-mounted |
| Supply voltage: | 24V DC rated(12~32V DC) |
| Company Info. |
| Stable Inertial Systems Ltd. |
| Verified Supplier |
| View Contact Details |
| Product List |
This product has built-in three-axis integrated high-precision
fiber optic gyro, high-precision quartz flexure accelerometer and
mobile mapping grade multi-mode and multi-frequency GNSS receiver
supporting autonomous BeiDou function. Through the advanced
intelligent combination navigation algorithm and Kalman filter,
optimized design for GNSS obstruction and multi-path interference,
it can realize high-precision heading, attitude, speed and position
measurement of moving carriers.
This inertial navigation system has a variety of sensor interfaces
such as GNSS/odometer/DVL/barometric altimeter, which can well meet
the needs of long-time, high-precision and high-reliability
navigation applications in complex environments such as urban
canyons, and can be used for the navigation and control of various
unmanned systems.
>Main technical parameters
System Real-time Accuracy | ||||||
Attitude Accuracy | Heading ≤0.04° (1σ); | |||||
Position Accuracy | Single-point positioning: horizontal ≤ 2m (50% CEP) | |||||
Speed Accuracy | 0.02m/s (Carrier speed less than 500m/s) | |||||
Alignment Time | Start timing after obtaining latitude, longitude and altitude position information. The alignment process duration is ≤5 minutes. | |||||
Inertial/ODO/DVL Combination | 0.5%×Miles traveled (depending on the accuracy of the external odometer) | |||||
Pure Inertial Specification | ||||||
Attitude Accuracy | Azimuth alignment accuracy: ≤0.1°sec (Φ) (1σ, Φ is local latitude) Horizontal attitude alignment accuracy: ≤0.006° (1σ) Azimuth hold accuracy: 0.02°/h (1σ) Horizontal Attitude Holding Accuracy: 0.02°/h (1σ) | |||||
Position Accuracy | Positioning accuracy: ≤1nmile/h(50%CEP) | |||||
Speed accuracy | Horizontal speed accuracy: ≤0.8m/s (1σ). | |||||
Main Device Characteristics | ||||||
Gyroscope | range | ±500°/s | Zero Bias Stability | ≤0.08°/h(1σ, 10s smooth) | ||
Accelerometer | range | ±20g | Zero Bias Stability | ≤30μg(1σ, 10s smooth) | ||
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 | ≤15W | |||||
Operating Temperature | -40℃~+55℃ | Transmission Rate | 9600~961200bps(configurable) | |||
Protection level | IP65 | User Mode | ||||
Physical Dimensions | ≤140mm×125mm×126mm | Vehicle-mounted (default), aircraft-mounted, ship-mounted | ||||
Weight | ≤2.75Kg | |||||

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