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| Categories | Electronic Gyroscope Sensor | 
|---|---|
| Brand Name: | Kacise | 
| Model Number: | KsINS-B | 
| 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 | 
| Packaging Details: | each unit has individual box and all boxes are packed in standard packages or customers requests available | 
| Align time: | ≤5min | 
| Speed accuracy: | In integrated navigation mode: sky speed ≤ 0.3m/s, horizontal speed ≤ 0.2m/s | 
| Heading maintenance accuracy: | 0.2° /h (pure inertia), 0.1° (integrated navigation) | 
| Company Info. | 
| Xi'an Kacise Optronics Co.,Ltd. | 
| Verified Supplier | 
| View Contact Details | 
| Product List | 
KsINS-B optical fiber strapdown inertial navigation system
product description:
The KsINS-B optical fiber strapdown inertial navigation system is a small general-purpose inertial navigation system using fiber optic gyroscopes and quartz flexible accelerometers. The system can be sensitive to the angular and linear motion of the UAV carrier, and output the carrier's position, speed, heading, angular rate, and linear acceleration information in real time. It can be combined with a satellite receiver to complete integrated navigation operations, which can meet the needs of various UAVs. Attitude control, navigation and positioning requirements.

Features:
● Small size, light weight, good production technology and high reliability
● Rich communication interfaces
● The output protocol is flexible and can be configured through test software
● Vibration reduction accessories are provided to meet the needs of harsh vibration environments
● Have a complete BIT strategy and passed the actual flight assessment
Application fields and application modes:
It has been maturely used in the fields of high-altitude airships, rotary-wing UAVs, and fixed-wing UAVs.
Performance indicators :
| Align time | ≤5min | 
| Position accuracy | Pure inertia: 2~5nmile/30min (CEP) Integrated navigation with satellite: height 10m; level 5m | 
| Speed accuracy | In integrated navigation mode: sky speed ≤ 0.3m/s, horizontal speed ≤ 0.2m/s | 
| heading alignment accuracy | ≤ 1.0° (1σ) (self-aligned) ≤ 0.1° (1σ) (dual antenna positioning, baseline 2 meters) | 
| Heading maintenance accuracy | 0.2° /h (pure inertia), 0.1° (integrated navigation) | 
| Attitude alignment accuracy | 0.05° (1σ) | 
| Attitude maintenance accuracy | 0.1° (pure inertia), 0.05° (integrated navigation) | 
Application environment :
| Working/storage temperature(℃) | -40℃ ~+60℃ /-45℃ ~+80℃ | 
| MTBF(h) | 30000h | 
| Dynamic Range | Angular velocity: ±300°/s; Acceleration: -25g~25g | 
| Mechanical properties | Endurance shock environment: half sine wave 20g, 11ms, Endurance Vibration Environment: 1. No shock absorption: GJB150.16A-2009 Figure C.3 Rear peak sawtooth wave 2. With shock absorption: GJB1032 random vibration spectrum | 
Physical properties:
| Dimensions | 135mm×135mm×84mm | 
| Installation dimensions | No shock absorption: M6 screw 121mm×121mm With shock absorption: M4 screw 121mm×121mm | 
| weight | ≤ 2.1kg | 
| waterproof level | IP67 | 
External Interface:
| powered by | 18V~36V DC | 
| Power consumption | ≤ 11W | 
| Input/output interface | RS-422×3 (multiplexing), RS-232×2 (multiplexing), LVTTL interface 1 CAN×2, network port×1, Pulse interface × 2, data storage 8G | 
| Data output frequency | ≤1000Hz | 
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