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| Categories | Electronic Gyroscope Sensor | 
|---|---|
| Brand Name: | Kacise | 
| Model Number: | KsINS-90L | 
| Certification: | certificate of explosion-proof, CE | 
| Place of Origin: | China (Mainland) | 
| MOQ: | 1pcs | 
| Payment Terms: | T/T, Western Union, MoneyGram | 
| Supply Ability: | 1000 Pieces per Week | 
| Delivery Time: | 5-8 working days | 
| Packaging Details: | each unit has individual box and all boxes are packed in standard packages or customers requests available | 
| Power consumption: | ≤ 40W | 
| weight: | 15kg | 
| Operating temperature: | -40℃~ +65℃ | 
| Company Info. | 
| Xi'an Kacise Optronics Co.,Ltd. | 
| Verified Supplier | 
| View Contact Details | 
| Product List | 
KsINS-90L type laser strapdown inertial navigation system
product description:
The KsINS-90L -type inertial navigation system is a standard high-precision laser strapdown inertial navigation system. It has the advantages of small size, light weight, high precision, and good reliability. It can meet the needs of long-term autonomous navigation in complex environments and is suitable for In various short-term navigation, integrated navigation, guidance and control and other fields. The heading alignment accuracy is better than ≤0.3mil (1σ), and the pure inertial navigation accuracy is better than 0.5nmile/h (CEP). The system can integrate satellite, radio, barometric altimeter, Doppler, odometer and other information to achieve high-precision integrated navigation.

Features:
● 15kg lightweight high-precision laser strapdown product, 40% cheaper than traditional products
●Using domestic high-precision spatial three-axis laser gyroscope and quartz flexible accelerometer
●Space three-axis laser gyroscope bias stability is better than 0.001°/h (1σ)
●Accelerometer bias stability is better than 30μg (1σ)
●Achieve static and dynamic base alignment, and can choose self-alignment, on-the-fly alignment or transfer alignment according to user needs
●It can be integrated with various information such as satellites, odometers, altimeters, star sensors, etc. for combined navigation, and the interface has strong scalability
Application fields and application modes:
Land use, navigation, drones, and can also be extended to other applications.
System performance:
| Car navigation | ship navigation | Drone navigation | Ship local datum | |
| Location (CEP) | ≤ 0.05%D, Odometer assist ≤ 0.1m, Differential Satellite Assist | ≤ 1nm/24h, Trip meter assist ≤ 0.1m, Differential Satellite Assist | ≤ 0.5nmile/h | ≤ 1m (relative) | 
| Speed(1σ) | ≤ 0.2m/s | ≤ 0.6m/s | ≤ 0.6m/s | ≤0.2m/s(relative) | 
| Heading(1σ) | ≤ 0.3mil | ≤0.1mil (relative) | ||
| Attitude (1σ) | ≤ 0.02° | ≤ 0.01° (relative) | ||
| Align time | 5min | 15-20min | 5min | 5min | 
System features:
| Power consumption | ≤ 40W | |
| size | 300mm (L) × 250mm (W) × 220mm (H) | |
| weight | 15kg | |
| Input voltage | 18V~32V | |
| Operating temperature | -40℃~ +65℃ | |
| Mechanical environment | impact | Half sine wave 30g, 11ms | 
| vibration | GJB150.16A-2009.C.3 | |
| Interface information | RS-422×2; RS-232×1; Ethernet interface; CAN bus interface; Odometer interface×1;Altimeter interface;Speedometer interface | |
Device performance:
| Top | Accelerometer | ||
| Bias stability | ≤ 0.001°/h,1σ | Offset Repeatability | ≤ 30μg, 1σ | 
| Offset Repeatability | ≤ 0.001°/h,1σ | Bias stability | ≤ 30μg, 1σ | 
| scaling factor | ≤ 5ppm, 1σ | Scaling factor repeatability | ≤ 50ppm, 1σ | 
| random walk | ≤ 0.0005°/ , 1σ | Scale factor stability | ≤ 50ppm, 1σ | 
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