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.
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.

KCD-3 Servo

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