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ProductCovers the entire application process for aviation/air defense and anti-missile weapon systems, from scientific research and design finalization to testing, evaluation, training, and exercises. MORE
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The company has a solid foundation of comprehensive personnel, rich experience, and technical advantages in the field of unmanned aerial vehicles and artificial intelligence applications. It actively cooperates with many domestic and foreign units to carry out joint research, forming a unique unmanned aerial vehicle research direction of "Jinpengda" with strong sustainability. MORE
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The company upholds the business philosophy of "integrity, dedication, pragmatism, and excellence", adheres to the mission of "innovation, transcendence, and leadership", creates a "renowned brand of unmanned aerial vehicles", and wholeheartedly provides users with comprehensive and full-cycle high-quality, efficient, and reliable services. MORE
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AboutGFA AVIATION TECHNOLOGY BEIJING Co..Ltd is a dual high-tech enterprise integrating R&D, production, and service of unmanned aerial vehicles and aero-engines. Established in 2012, with a registered capital of 67.35 million yuan, it is located in Zhongguancun Science Park - Fangshan Park, and has complete R&D and production facilities. MORE
KFS-3B integrated control and navigation unit

Technical Parameters
Power Supply | +20V~﹢32V DC |
Communication Interface | 8-channel RS-422 (including 2 channels expansion) |
2-channel CAN | |
2-channel RS-232 | |
Analog Input | 4-channel (16bit A/D) |
Discrete Input | 4-channel |
Discrete Output | 12-channel (0 and 28V signals configurable) |
Servo Loop | 4-channel (KCD-3 servo) |
Three-axis Acceleration | ﹣18g~﹢18g |
Three-axis Angular Rate Range | ﹣300°/s~﹢300°/s |
Zero Drift | ≤12°/h |
Positioning Accuracy | ≤20m |
Air Pressure Altitude Range | -400m~18000m |
GNSS Receiver | 2 units |
Operating Temperature | ﹣55℃~﹢80℃(﹣40℃ startup,﹣55℃ operation) |
Storage Temperature | ﹣40℃~﹢80℃ |
Shock | 15g (three axial directions) |
The KFS-3B flight control and navigation unit consists of a MEMS inertial measurement unit, a GNSS receiver, a barometric pressure sensor, and a main controller based on a high-performance ARM processor. Based on sensor measurements of status information, the flight control and navigation unit pre-sets flight paths and commands, performing real-time calculations and controlling the aircraft to achieve flight control and navigation functions.
The MEMS inertial measurement unit measures and collects the carrier's raw inertial navigation data, including rate gyro data and accelerometer data. The GNSS receiver obtains GNSS position and velocity data; dual GNSS is used to improve performance and reliability. The barometric pressure sensor receives total and static pressure from the airspeed tube, calculating parameters such as true airspeed, indicated airspeed, and flight altitude. Inertial navigation and GNSS combined navigation calculations are performed, and then the carrier's control surfaces are controlled to achieve carrier climbing, descending, and turning.
Other Content
KFS-4 integrated control and navigation unit
The KFS-4 integrated control and navigation unit uses a high-speed, high-performance ARM as its main control chip, and incorporates a MEMS inertial measurement unit, GNSS receiver, atmospheric pressure sensors, etc., to construct a digital control system. Based on data from sensor measurements, it performs integrated navigation calculations, flight path prediction, and command control, calculating and controlling the servo output in real time to achieve flight control and navigation functions. In addition, the KFS-4 integrated control and navigation unit is designed with abundant communication interface resources such as RS422, CAN, and USB, facilitating future expansion and upgrades.
The KCD-3 servo motor consists of a maxon imported motor, a low-backlash harmonic reducer, and a precision non-linear wound angle sensor.
Image Display
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