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XCD1G XCD-7 XCD-160 XCD-220
Fixed-wing unmanned aerial vehicle
GHQ-400 GHQ-600
Compound-wing UAV
FCD-30 FCQ-150
Drone Hive
FCDH-36(S)A XCDH-2(S)A
Simulation Testing Services
Visual Simulation Platform
HIL Simulation Test Platform
Fixed-wing UAV simulation training system
FPV Drone Simulation Training System
Experimental Integrated Control and Management System
Command and Control System Products
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
Avionics System Products
Flight Control Computer Products
LKD-KFS-103 LKD-KFS-120A LKD-KFS-120C LKD-KFS-120D LKD-KFS-220 LKD-KFS-300 LKD-KFS-501
Mission Computer Products
3588 Person Machine (Edge Intelligence Terminal)
Avionics equipment
LKD-TXD-005A LKD-TXD-006A LKD-HQD-002 LKD-XFJ-001 LKD-FFS-100
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Hang-flight test
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Product Classification
Drone products
Simulation Testing Services
Command and Control System Products
Avionics System Products
Drone services
Multirotor drone
XCD1G
XCD1G
XCD-7
XCD-7
XCD-160
XCD-160
XCD-220
XCD-220
Fixed-wing unmanned aerial vehicle
GHQ-400
GHQ-400
GHQ-600
GHQ-600
Compound-wing UAV
FCD-30
FCD-30
FCQ-150
FCQ-150
Drone Hive
FCDH-36(S)A
FCDH-36(S)A
XCDH-2(S)A
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
Current location：
LKD-FFS-100

LKD-FFS-100

The simulation computer is based on the company’s current mainstream flight control architecture.

It is used to support system-level simulation for the company’s various flight control series, comprehensively covering all interface types across different aircraft models. By pairing a simulator with any flight controller, a closed-loop simulation system can be readily established.

Features And Advantages

FEATURES AND ADVANTAGES

  • 16V~29V wide-voltage power supply

    Power supply surge resistance and reverse polarity protection capabilities

  • Simulator and flight control aircraft

    Independent power supply button

  • External Power Supply Voltage Monitoring

    Power monitoring, with automatic shutdown capability in case of overvoltage, undervoltage, or overpower conditions.

  • Serial port, CAN, PWM

    Discrete signals and various other types of interfaces

Performance Parameters

PERFORMANCE PARAMETERS

  • Power Supply – Supply Voltage

    DC 16V~29V

  • Power Supply – Total System Power Consumption

    ≤10W

  • Power Supply – Protection Capability

    Reverse-polarity and surge-protection circuitry

  • Processor - Processor

    CPU architecture: XC7Z020 series, dual-core ARM Cortex-A9
    Main Frequency: 666.6 MHz

  • Processor–Storage Resources

    FRAM: 256 Kbit
    FLASH: 32MB
    EEPROM: 256 Kbit
    DDR: 512 Mbytes
    eMMC: 16 Gbytes

  • Serial Port – RS232/422/485

    Number of channels: 2 channels
    Baud Rate: Software Configuration
    Mode: Software Configuration
    RS232 baud rate: 1 Mbps
    RS485/422 baud rate: 10 Mbps

  • Serial Port - RS232/422

    Number of channels: 15 channels
    Baud Rate: Software Configuration
    Mode: Software Configuration
    RS232 baud rate: 1 Mbps
    RS422 rate: 10 Mbps

  • Functional Interface – CAN Interface

    Number of channels: 2 channels
    Rate: ≤1 Mbps

  • Functional Interface – Network Interface

    Number of channels: 2 channels
    Feature: 100 Mbps Ethernet port

  • Functional Interface – PWM Interface

    Number of channels: 24 channels
    Features: The software is configurable in terms of direction.

  • Functional Interface – Analog Signal Acquisition

    Number of channels: 4 channels
    Range: ±10 VDC

  • Functional Interface – Analog Output

    Number of channels: 8 channels
    Range: ±10 VDC

  • Functional Interface – Digital I/O Interface

    Number of channels: 8 channels
    Features: The software is configurable in terms of direction.
    Voltage: 5V/GND

  • Functional Interface – Discrete Input

    Number of channels: 4 channels
    Features: 28V/ON and GND/ON, hardware-configurable

  • Functional Interface – Discrete Output

    Number of channels: 8 channels
    Features: 28V/ON and GND/ON, hardware-configurable

  • Environmental Adaptability – Operating Temperature

    -40℃~55℃

  • Environmental Adaptability – Storage Temperature

    -40℃~55℃

Application Scenarios

APPLICATION SCENARIOS
It can be used as a complementary simulation device for the company’s in-house flight control system, or deployed as a standalone simulation computer.

It can be used as a complementary simulation device for the company’s in-house flight control system, or deployed as a standalone simulation computer.

It can be used as a complementary simulation device for the company’s in-house flight control system, or deployed as a standalone simulation computer.

It can be used as a complementary simulation device for the company’s in-house flight control system, or deployed as a standalone simulation computer.

It can be used as a complementary simulation device for the company’s in-house flight control system, or deployed as a standalone simulation computer.

It can be used as a complementary simulation device for the company’s in-house flight control system, or deployed as a standalone simulation computer.