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Advanced Visual Inertial Navigation System For Aircraft Takeoff And Landing With Weight ≤2.0kg
Advanced Visual Inertial Navigation System For Aircraft Takeoff And Landing With Weight ≤2.0kg
Advanced Visual Inertial Navigation System For Aircraft Takeoff And Landing With Weight ≤2.0kg
Advanced Visual Inertial Navigation System For Aircraft Takeoff And Landing With Weight ≤2.0kg
Specifications
Brand Name :
Kacise
Model Number :
KsINS-02
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
Field of view(visible light) :
57.80°×34.50°
System preparation :
Static Base Alignment, Alignment Time 5 Minutes
weight :
≤2.0kg
Navigation accuracy (takeoff) :
1.0m
Navigation accuracy (cruise) :
20m+1%H
Field of view(infrared) :
35.83°×27.26°
Storage temperature :
-45℃ ~+65℃
Power Requirement :
28V, Adjustable Range 24V~36V
Description

Product Description:

Designed as an airborne inertial visual navigation system, the KsINS-02 integrates inertial navigation, visible light camera, infrared camera, and an AI data processing circuit. By leveraging the principles of optical imaging and inertial measurement, it provides UAVs with a wealth of information, including inertial/visual combined attitude, speed, position, angular velocity, acceleration, and more. This product incorporates artificial intelligence technology, revolutionizing image and video recognition within the field of drone navigation. Through the fusion of inertial/machine vision multi-information, it achieves high-precision real-time measurement of aircraft motion parameters independent of satellites, offering a holistic solution for autonomous guidance and navigation throughout the entire mission profile, encompassing takeoff, cruising, and landing.Advanced Visual Inertial Navigation System For Aircraft Takeoff And Landing With Weight ≤2.0kg

Features:

● Provide autonomous navigation information for the entire mission profile of UAV take-off, cruise and landing

● Autonomous recognition of airport runways all day and night based on AI, adaptable to emergency landings at unfamiliar airports

● Front view and downward view can be installed flexibly and can be expanded to receive image information of loads such as pods.

● Suitable for Gobi, desert, mountain, city and other scenes

● Does not rely on satellites and dedicated pre-made maps

Product advantages:

● Integrated design of imaging and navigation

● Strong adaptability to the airborne environment

● High-precision inertial/visual information fusion

● Visible light and infrared images are fused and output as SDI standard video

● Target detection results are displayed in real time

Technical Parameters:

Performance indicators :

take off Cruise section Take-off and landing stage
Action range Before leaving the ground 1km~8km (relative altitude) The forward distance is 5km~ Stop (the runway width is not less than 45m)
Navigation accuracy 1.0m(1σ,lateral accuracy) 20m+1%H (1σ, horizontal positioning accuracy,H is the height of the aircraft relative to the ground) 1.0m+1‰ D (1σ, lateral accuracy, D is horizontal distance between the aircraft and the runway endpoint)

Application environment :

Operating temperature -40℃ ~+60℃
Storage temperature -45℃ ~+65℃
System preparation

static base alignment,

Alignment time 5 minutes
Field of view visible light 57.80°×34.50°
infrared 35.83°×27.26°

Physical properties:

Length*width*height 179mm×140mm×126mm
weight ≤ 2.0kg
Front view installation dimensions 10-M3×8mm threaded hole
Installation dimensions as viewed from below 4-M4×8mm threaded hole

External Interface:

Power Requirement 28V, adjustable range 24V~36V
Power consumption ≤ 40W

Electrical Interface

 user connector F104Z19K092-140, realizing power supply and communication
Debug connector F104Z19K086-240, realize software upgrade
2-way standard SMA connector 1920×1080@30Hz format SDI video output

Communication Interface

 RS422 serial port Inertial navigation information input 200Hz
RS422 serial port Flight control command input 5Hz
Inertial/visual integrated navigation information output 100Hz

Support and Services:

If you experience any issues with the product, please contact us for further assistance. Our team will be happy to help you troubleshoot any problems you're experiencing and provide a resolution.

We also provide a range of additional services, such as product installation, maintenance, and repair. If you require any of these services, please contact us and we will be happy to discuss your requirements.

Packing and Shipping:

The visual inertial navigation system is packaged and shipped in a sturdy cardboard box that is sealed with adhesive tape. The box is labeled with the product name and a detailed product description. Inside the box, the sensor is securely wrapped in bubble wrap and foam padding to protect it from any damage during transit.
Product tags

inertial navigation system aircraft

,

ride height sensor

,

navigation system in aircraft
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Advanced Visual Inertial Navigation System For Aircraft Takeoff And Landing With Weight ≤2.0kg

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Product Detail
Brand Name :
Kacise
Model Number :
KsINS-02
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
Contact Supplier
Advanced Visual Inertial Navigation System For Aircraft Takeoff And Landing With Weight ≤2.0kg
Advanced Visual Inertial Navigation System For Aircraft Takeoff And Landing With Weight ≤2.0kg

Xi'an Kacise Optronics Co.,Ltd.

Verified Supplier
7 Years
Shaanxi
Since 2008
Business Type :
Manufacturer
Main Products :
Fluid Level Meter, Water Quality Sensor, Precision Pressure Sensor
Total Annual :
8000000-10000000
Employee Number :
100~150
Certification Level :
Verified Supplier
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