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.
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.
