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.
View DetailsMy company is a technology enterprise that integrates the research and development, production, and service of unmanned aerial vehicles and aero-engine systems.
View DetailsKFS-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.
View DetailsKFS-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.
View DetailsThe KCD-3 servo motor consists of a maxon imported motor, a low-backlash harmonic reducer, and a precision non-linear wound angle sensor.
View DetailsThe KCD-4 servo motor consists of a maxon imported motor, a low-backlash harmonic reducer, and a precision non-linear wound angle sensor.
View DetailsTSD-3 telemetry and control station
Capable of multi-target control, with backup remote control link.
View DetailsTSD-2 telemetry and control station
Main and backup dual links allow for multi-target control.
View DetailsCKS-313T1 test and control radio station
The CKS-313T1 telemetry and control station can be used as an airborne station or a ground station. It establishes a wireless communication link between the airborne station and the ground station, and then uploads and downloads data according to the predetermined time sequence logic. It also has the capability to communicate with multiple airborne stations from one ground station (it can connect up to 20 airborne stations).
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