Product Description:
As an airborne inertial visual navigation product, KsINS-02 is
predominantly composed of inertial navigation, visible light
camera, infrared camera, and an AI data processing circuit.
Grounded in the principles of optical imaging and inertial
measurement, it supplies UAVs with a comprehensive array of
information, including inertial/visual combined attitude, speed,
position, angular velocity, acceleration, and more. Incorporating
artificial intelligence technology, it brings revolutionary changes
to image and video recognition within the domain of drone
navigation. Through the fusion of inertial/machine vision
multi-information, it achieves high-precision real-time measurement
of aircraft motion parameters, eliminating the need for satellite
dependence. In this context, it delivers a comprehensive solution
for autonomous guidance and navigation throughout the entire
mission profile, spanning 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:
We provide quick solutions and support for technical issues,
including troubleshooting, software installation and configuration,
hardware repair, and more.
We also provide regular maintenance services, such as cleaning and
calibration, to ensure that your sensor is functioning properly.
If you need further assistance, please don’t hesitate to contact
us.
Packing and Shipping:
The box will contain the sensor and all accessories needed for
installation. The box will be well padded to protect the contents
during transit.
The box will be securely sealed and labeled with the address of the
customer. Shipping will be done via a reputable carrier with
tracking number provided to the customer.
