Flight Control System (FCS)
FCS is a core technology for drone design, which is required for controlling the location, pose, and flight path of the drone
Ability to self-design core modules (AHRS, FC)
Controller Customization, Tracking and analysis of flight logs
Able to Customize and Select FCS Modes
Classify | GD FCS | FCS (Company ‘D’) | FCS (Company ‘F’) |
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Flight Mode |
Manual mode (Manual control) P-Mode (Positioning) Atti Mode (Altitude Hold) F-Mode (Directional Maintenance Mode) |
Manual mode (Manual control) Manual + GPS Mode Atti Mode (Altitude Hold) Atti + GPS Mode Auto Mode Obstacle evasion mode |
Manual mode (Manual control) Manual + GPS Mode Atti Mode (Altitude Hold) Atti + GPS Mode Mission Mode OFF BOARD |
RTH (Return To Home, Automatic Return) |
Low Voltage RTH Failsafe RTH (In case of signal loss) |
Low Voltage RTH Failsafe RTH (In case of signal loss) Over Range RTH (When flying out of range) |
Low Voltage RTH Failsafe RTH (In case of signal loss) Over Range RTH (When flying out of range) |
Aircraft design platform |
4-Rotor, 6-Rotor, 8-Rotor |
4-Rotor, 6-Rotor, 8-Rotor |
4-Rotor, 6-Rotor, 8-Rotor |
Supported communication methods |
Own Method : Lightbridge 2, DR16 Universal Method : S-Bus |
Universal Method : S-Bus |
Universal Method : S-Bus |
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AHRS : Inertial Measurement Device
Attitude and heading reference system
Calculation of aircraft status (position, altitude, direction, etc.)
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FCC : Flight Control Device
Flight Control Computer
Collects various data to control position and angle
Ground Control System (GCS)
Autonomous flight & Real-time flight path control
Map data processing & Pre-analysis of flight path
Geofence (When necessary, create no-fly zones)
