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| Categories | Electronic Gyroscope Sensor |
|---|---|
| Brand Name: | Kacise |
| Model Number: | KsINS-01 |
| Place of Origin: | China (Mainland) |
| Certification: | certificate of explosion-proof, CE |
| MOQ: | 1pcs |
| Packaging Details: | each unit has individual box and all boxes are packed in standard packages or customers requests available |
| Delivery Time: | 5-8 working days |
| Payment Terms: | T/T, Western Union, MoneyGram |
| Supply Ability: | 1000 Pieces per Week |
| Spatiotemporal synchronization accuracy in case of satellite rejection (RMS): | 5m/5ns |
| Dynamic Range: | Speed: -2000m/s ~ 2000m/s; Acceleration: -30g ~ 30g; Acceleration: -5g/s ~ 5g/s. |
| Power Requirement: | 18V~36V DC, Power Consumption ≤ 30W, Allowed Power Interruption Is No More Than 5ms |
| Data output frequency: | 10Hz (typical) |
| Input/output interface: | 2 RS-422, 1 RS-232, 1 100M Ethernet |
| Communication distance: | 100km |
| Installation dimensions: | 160mm X 150mm |
| Working/storage temperature(℃): | -55℃ ~+70℃ |
| Company Info. |
| Xi'an Kacise Optronics Co.,Ltd. |
| Verified Supplier |
| View Contact Details |
| Product List |
Precision, velocity and balance are key to any moving object. When it comes to complex vehicles, like airplanes, autonomous vehicles, ships, spacecraft, submarines and even unmanned aerial vehicles (UAVs), the need for an accurate system that helps maintain and control perfect movement is essential. With the help of inertial navigation systems, moving vehicles can accomplish their tasks safely and precisely without using GPS.
The KsINS-01 integrated communication and guidance cooperative navigation system has been developed with a focus on UAV swarm formation flight. It seamlessly combines satellite navigation and data links to offer precise spatio-temporal references for UAVs. The system incorporates Beidou third-generation B1 and B3 frequency signal reception, enabling inter-node networking communication and high-precision space-time synchronization capabilities. Achieving a spatio-temporal synchronization accuracy of better than 0.1m/1ns under satellite effective conditions, and 5m/5ns under satellite rejection conditions.
● High-precision spatio-temporal synchronization between nodes based on carrier difference
● High-precision spatio-temporal synchronization between nodes under satellite rejection conditions
● In-depth integrated design of satellite navigation and data link
● Highly reliable networking and data transmission between nodes
Performance indicators :
| Satellite positioning accuracy (2σ) | Level: 6m, elevation: 8m |
| Data link working frequency band | 3.4GHz~3.6GHz |
| Frequency hopping rate | 80000 hops/s |
| Communication distance | 100km |
| Communication rate | 200kbps |
| Number of supported nodes | 64 |
Spatiotemporal synchronization accuracy when satellites are available (RMS) | 0.1m/1ns |
Spatiotemporal synchronization accuracy in case of satellite rejection (RMS) | 5m/5ns |
Application environment :
| Working/storage temperature(℃) | -55℃ ~+70℃ |
| Dynamic Range | Speed: -2000m/s ~ 2000m/s; Acceleration: -30g ~ 30g; acceleration: -5g/s ~ 5g/s. |
| Mechanical properties | Endurance shock environment: half sine wave 20g, 11ms Endurance vibration environment: typical drone vibration environment |
Physical properties:
| Dimensions | 160mm x 150mm x 56mm |
| Installation dimensions | 160mm x 150mm |
| weight | Host ≤ 12.5kg |
External Interface:
| Power Requirement | 18V~36V DC, power consumption ≤ 30W, allowed power interruption is no more than 5ms |
| Input/output interface | 2 RS-422, 1 RS-232, 1 100M Ethernet |
| Data output frequency | 10Hz (typical) |
The INS is packaged in a cardboard box with foam padding to protect the product during transit. The box is labelled with the product name and the customer's shipping address. The box is then sealed with packing tape and shipped to the customer via a reputable third-party shipping provider.
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