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It covers the entire application process of multi-system scientific research, type approval, inspection, evaluation, training and exercises. MORE -
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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GFA 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 72.35 million yuan, it is located in Zhongguancun Science Park - Fangshan Park, and has complete R&D and production facilities. MORE
The Leiting turbofan engine series is mainly used in small and medium-sized UAVs, cruise weapons, air-launched decoys, etc., and can also be used in civilian light aircraft and gliders. It features high performance indicators, stable and reliable operation, good high-altitude performance, high integration, convenient use and maintenance, and high cost-effectiveness. Existing models include the Leiting 150, Leiting 125, Leiting 90, and Leiting 40.
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The Leiting turbofan engine series is mainly used in small and medium-sized UAVs, cruise weapons, air-launched decoys, etc., and can also be used in civilian light aircraft and gliders. It features high performance indicators, stable and reliable operation, good high-altitude performance, high integration, convenient use and maintenance, and high cost-effectiveness. Existing models include the Leiting 150, Leiting 125, Leiting 90, and Leiting 40.
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The Leiting turbofan engine series is mainly used in small and medium-sized UAVs, cruise weapons, air-launched decoys, etc., and can also be used in civilian light aircraft and gliders. It features high performance indicators, stable and reliable operation, good high-altitude performance, high integration, convenient use and maintenance, and high cost-effectiveness. Existing models include the Leiting 150, Leiting 125, Leiting 90, and Leiting 40.
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KFS-3A integrated flight control and navigation unit
My company is a technology enterprise that integrates the research and development, production, and service of unmanned aerial vehicles and aero-engine systems.
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My company is a technology enterprise that integrates the research and development, production, and service of unmanned aerial vehicles and aero-engine systems.
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KFS-3B integrated control and navigation unit
The KFS-3B flight control and navigation unit consists of a MEMS inertial measurement unit, a GNSS receiver, an atmospheric pressure sensor, and a main controller based on a high-performance ARM. The flight control and navigation unit uses sensor measurements to determine the flight path and commands, performing real-time calculations and controlling the aircraft to achieve flight control and navigation. It uses a MEMS inertial measurement unit to measure and collect the carrier's raw inertial navigation data, including rate gyro data and accelerometer data. A GNSS receiver obtains GNSS position and velocity data; dual GNSS is used to improve performance and reliability. An atmospheric pressure sensor receives total and static pressure from the airspeed tube to calculate parameters such as true airspeed, indicated airspeed, and flight altitude. Inertial navigation and GNSS combined navigation calculations are performed, and then the aircraft's control surfaces are controlled to achieve climbing, descending, and turning.
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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.
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The KCD-3 servo motor consists of a maxon imported motor, a low-backlash harmonic reducer, and a precision non-linear wound angle sensor.
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The KCD-4 servo motor consists of a maxon imported motor, a low-backlash harmonic reducer, and a precision non-linear wound angle sensor.
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