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.
KFS-3A integrated flight control and navigation unit

Technical Parameters


Pitch Angle Accuracy ≤1º (GNSS combined)
Roll Angle Accuracy ≤1º (GNSS combined)
Three-axis Acceleration Range ±18g
Three-axis Angular Rate Range ±300°/s
Combined Position Accuracy ≤10m (GNSS combined)
Barometric Altitude Range -400m~18000m
Airspeed Range 50km/h~1400km/h
Rate of Climb Range ±200m/s
Digital Interface RS-422 serial port, 8 channels
RS-232 serial port, 2 channels
Analog Interface Analog input (16-bit A/D, ±10V), 4 channels
Discrete Interface Discrete input 4 channels
Discrete output 12 channels
28VDC level signal
Servo Loop ≤5 channels
Operating Temperature -55℃~60℃ (-40℃ startup)
Power Supply ﹢20~﹢32VDC, power consumption ≤300W

Other Content


KCD-3 Servo

My company is a technology enterprise that integrates the research and development, production, and service of unmanned aerial vehicles and aero-engine systems.

TSD-3 telemetry and control station

Capable of multi-target control, with backup remote control link.

Image Display