Stable Inertial Systems Ltd.
| Payment Terms | D/A,L/C,D/P,T/T,Western Union |
| Delivery Time | 6-8 weeks |
| Drift rate | Low drift rate |
| Navigation type | Inertial Navigation |
| Maintenance | Low maintenance requirements |
| Pitch and roll | ≤0.01° (1σ) |
| Type | Inertial Navigation System |
| Heading | ≤0.05° (1σ) |
| Bias Stability | ≤0.15°/h |
| Brand Name | SI |
| Model Number | SI-FINS40S-S2 |
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Product Specification
| Payment Terms | D/A,L/C,D/P,T/T,Western Union | Delivery Time | 6-8 weeks |
| Drift rate | Low drift rate | Navigation type | Inertial Navigation |
| Maintenance | Low maintenance requirements | Pitch and roll | ≤0.01° (1σ) |
| Type | Inertial Navigation System | Heading | ≤0.05° (1σ) |
| Bias Stability | ≤0.15°/h | Brand Name | SI |
| Model Number | SI-FINS40S-S2 | ||
| High Light | Precision Fiber Optic Inertial Navigation System ，Robust Operation Inertial Navigation System ，Inertial Navigation System Navigation for UAVs | ||
This product features a high-precision three-axis integrated fiber optic gyroscope, a compact quartz flexible accelerometer, and a mobile survey-grade multi-mode multi-frequency GNSS receiver with autonomous Beidou support. Utilizing advanced intelligent composite navigation algorithms and Kalman filtering, it is optimized for GNSS occlusion and multipath interference scenarios, enabling high-precision measurement of heading, attitude, velocity, and position for mobile platforms.
The INS also has a variety of sensor interfaces, which can meet the requirements of long-term, high-precision and high-reliability navigation in complex environments such as urban canyon, and can be used for navigation and control of various platform systems.
Main technical parameters
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System Real-time Accuracy |
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Attitude Accuracy |
Heading ≤0.05° (1σ); |
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Position Accuracy |
Single-point horizontal positioning: ≤1.5m (1σ) |
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Speed Accuracy |
Horizontal velocity ≤0.03 m/s (1σ), vertical velocity ≤0.05 m/s (1σ)
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Alignment Time |
Start timing after obtaining latitude, longitude and altitude position information. The alignment process duration is ≤5 minutes. |
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Inertial/ODO/DVL Combination |
0.5%×Miles traveled (depending on the accuracy of the external odometer) |
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Pure Inertial Specification |
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Attitude Accuracy |
Azimuth alignment accuracy: ≤0.5°sec (Φ) (1σ, Φ is local latitude) Horizontal attitude alignment accuracy: ≤0.01° (1σ)Azimuth hold accuracy: 0.15°/h (1σ) Horizontal Attitude Holding Accuracy: 0.03°/h (1σ) |
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Position Accuracy |
Positioning accuracy: ≤5.0nmile/h(50%CEP) |
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Speed accuracy |
Horizontal speed accuracy: ≤5.0m/s(1σ). |
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Main Device Characteristics |
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Gyroscope |
range |
±500°/s |
Zero Bias Stability |
≤0.15°/h(1σ, 10s smooth)
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Accelerometer |
range |
±15g |
Zero Bias Stability |
≤30μg(1σ, 10s smooth)
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Physical Characteristic |
Interface Characteristics |
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Supply voltage |
24V DC rated(12～32V DC) |
Interface method |
4 serial ports (RS232 or RS422) Support PPS, EVENTMARK input/output |
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Power Consumption |
≤18W |
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Operating Temperature |
-40℃~+60℃ |
Transmission Rate |
9600～961200bps(configurable) |
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Protection level |
IP65 |
User Mode |
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Physical Dimensions |
≤100mm×100mm×108mm |
Vehicle-mounted (default), aircraft-mounted, ship-mounted
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Weight |
≤1.4Kg |
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Company Details
Business Type:
Manufacturer,Seller
Year Established:
1997
Total Annual:
5000000-10000000
Employee Number:
500~1000
Ecer Certification：
Verified Supplier
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