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XCD-160
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XCD-220
Fixed-wing unmanned aerial vehicle
GHQ-400
GHQ-400
GHQ-600
GHQ-600
Compound-wing UAV
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FCD-30
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FCQ-150
Drone Hive
FCDH-36(S)A
FCDH-36(S)A
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XCDH-2(S)A
Visual Simulation Platform
HIL Simulation Test Platform
Fixed-wing UAV simulation training system
FPV Drone Simulation Training System
Experimental Integrated Control and Management System
Cloud Platform Management Software (Lingkong Cloud)
General-purpose command and control software for small and medium-sized unmanned aerial vehicles
Command and Control Software for Large Fixed-Wing Unmanned Aerial Vehicles
Unmanned Aerial Vehicle Ground Inspection System
Portable UAV Command and Control System
Unmanned Aerial Vehicle Command and Control Module System
Unmanned Aerial Vehicle Transport Module System
Integrated UAV Transport and Command-and-Control Modular System
Flight Control Computer Products
LKD-KFS-103
LKD-KFS-103
LKD-KFS-120A
LKD-KFS-120A
LKD-KFS-120C
LKD-KFS-120C
LKD-KFS-120D
LKD-KFS-120D
LKD-KFS-220
LKD-KFS-220
LKD-KFS-300
LKD-KFS-300
LKD-KFS-501
LKD-KFS-501
Mission Computer Products
3588 Person Machine (Edge Intelligence Terminal)
3588 Person Machine (Edge Intelligence Terminal)
Avionics equipment
LKD-TXD-005A
LKD-TXD-005A
LKD-TXD-006A
LKD-TXD-006A
LKD-HQD-002
LKD-HQD-002
LKD-XFJ-001
LKD-XFJ-001
LKD-FFS-100
LKD-FFS-100
Hang-flight test
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LKD-KFS-120C

LKD-KFS-120C

The LKD-KFS-120C flight control and management computer is based on the LKD-KFS-120A flight control and management computer.

A flight control and management computer has been developed, compliant with the environmental test requirements for military equipment specified in GJB 150A‑2009, including tests for damp heat, mold, and salt spray. The product features enhanced connectivity, with additional Gigabit Ethernet ports, serial interfaces, discrete input channels, CAN interfaces, and Pt1000/Pt100 temperature‑sensing interfaces, while its atmospheric data system design parameters have been refined. It is a versatile flight control and management solution suitable for various types of unmanned aerial vehicles, such as multirotors, fixed-wing aircraft, and vertical takeoff and landing (VTOL) platforms.

Features And Advantages

FEATURES AND ADVANTAGES

  • Complies with GJB150A-2009

    Environmental test methods for military equipment specify requirements for tests such as damp heat, mold, and salt spray.

Performance Parameters

PERFORMANCE PARAMETERS

  • Steady-state voltage

    DC 28 V, range DC 18 V to 36 V

  • Total system power consumption

    ≯200,000

  • CPU clock speed

    766.6 MHz

  • RAM

    512MB @ DDR3

  • FLASH

    32MB @ QSPI

  • F-RAM

    512KB

  • Data storage

    32GB@eMMC

  • Inertial navigation

    Three-axis gyroscope, three-axis accelerometer, three-axis magnetic compass

  • Static pressure sensor

    160 kPa

  • Dynamic pressure sensor

    ±6 kPa and ±25 kPa

  • Positioning and orientation function

    Supports GPS, GLONASS, Galileo, and BeiDou.

  • Analog Input

    Channel 4 ±10 VDC

  • RS232/RS422 isolation

    Route 23

  • RS232/422/485 isolation

    Route 2

  • Discrete Input

    Channel 8: Power/On or GND/On

  • Discrete Output

    Channel 8: Power/On or GND/On

  • Isolated CAN

    Route 2

  • Isolated CAN-FD interface

    Route 4

  • Gigabit Ethernet

    Route 2

  • Temperature Acquisition

    Route 2

  • Environmental adaptability

    Operating temperature: -40°C to 55°C
    Storage temperature: -40°C to 65°C

Application Scenarios

APPLICATION SCENARIOS
Multirotor, fixed-wing, and vertical takeoff and landing drones, among other types.

Multirotor, fixed-wing, and vertical takeoff and landing drones, among other types.

Multirotor, fixed-wing, and vertical takeoff and landing drones, among other types.

Multirotor, fixed-wing, and vertical takeoff and landing drones, among other types.

Multirotor, fixed-wing, and vertical takeoff and landing drones, among other types.

Multirotor, fixed-wing, and vertical takeoff and landing drones, among other types.