Xi'an Kacise Optronics Co.,Ltd.
Kacise, understanding your automation needs.
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The KsINS-02 serves as an airborne inertial visual navigation system, comprising elements such as inertial navigation, visible light camera, infrared camera, and AI data processing circuit. By combining principles of optical imaging and inertial measurement, it furnishes UAVs with comprehensive information including inertial/visual combined attitude, speed, position, angular velocity, acceleration, and more. This product incorporates artificial intelligence technology, introducing revolutionary advancements in image and video recognition into the realm of drone navigation. Through the fusion of inertial/machine vision multi-information, it achieves high-precision real-time measurement of aircraft motion parameters without relying on satellites, presenting a comprehensive solution for autonomous guidance and navigation across the entire mission profile, from takeoff to cruising and landing.
● 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
Performance indicators :
| take off | Cruise section | Take-off and landing section | |
| 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 | ||
The inertial navigation system will be carefully packaged in a bubble wrap mailer.