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FC800 Flight Control

SKU: FC800

Tri-redundancy ,Ultra-high Integration ,RTK&PPK&Dual-antenna Direction Finding。

FC800 series professional level, ultra high reliable flight control and navigation system with integrated micro- combination navigation system, Novatel high precision real- time differential GPS module (position accuracy up to centimeter), dual antenna orientation module and digital datalink ( Optional), through highly integrated with simplifying external wiring, further improve system reliability and stability. It is especially suitable for 100 kg medium range full- automatic take- off and landing fixed- wing, vertical take- off and landing fixed- wing and tilt- rotor drones.

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    Performance index:

    Parameter index
    Attitude accuracy 0.35°
    Course accuracy 0.08° (2m baseline)
    RTK positioning accuracy 1cm+1ppm
    Angular velocity measurement range ±450° /s
    Accelerometer measurement range ±6g
    Height measuring range – 500m ~ 10000m
    Voltage monitoring range 0 ~ 52V
    Steering gear update frequency 50Hz
    Engine speed monitoring range 0 ~ 20000RPM
    Communication interface RS- 232C
    Voltage monitoring channel 2 channels
    Engine speed monitoring channel 2 channels
    PWM control channel 9 channels
    Digital output channel 3 channels(PWM programmable)
    Expansion serial port 3 channels(connect to RTK, mission payload, etc.)
    Sbus input range 1 channel
    Electrical parameters
    Power supply voltage DC4.5- 9.0V
    DC7.0~36V
    Power consumption < 6W
    Physical parameters
    Weight ≤480g
    Dimensions(mm) 153*98*47.5
    Environment parameters
    Working temperature -40℃~ 85℃
    Storage temperature -40℃~ 85℃

    External dimension:

    FC800: Vertical take-off and landing fixed-wing flight control and navigation system

    FC810: Tilt-rotor flight control and navigation system

    FC850: Conventional fixed-wing (hand throwing, ejection, parachute landing, sprinting take-off and

    landing) flight control and navigation system

    Features:

    The internal integrated with tri- redundancy inertia device, the main redundancy is ADI high- quality gyro and accelerometer, and can switch the standby redundancy in real time according to the working mode, with the advantages of high measurement accuracy and high reliability;

    Integrated with dual redundancy satellite navigation system, Novatel high precision real- time differential GPS module (RTK position accuracy up to centimeter) and the internal single- point positioning GPS module is redundant with each other, and the system automatically selects GPS data with better positioning status;

    Integrated with high precision dual antenna orientation module, heading measurement precision: 0.5° (0.5m baseline);

    The perfect emergency protection mechanism can protect against low voltage, low oil quantity, low speed, abnormal posture, abnormal height, low GPS position accuracy, navigation system failure, exceeding of safety and control radius ranges, remote control failure, etc.;

    It can preset 100 landing points, and automatically land nearby according to the emergency;

    Provide 8 user routes, each route can add 800 waypoints;

    It can automatically generate hovering route, hovering center, hovering radius, and number of hovering circles can be set;

    The flight information and mission information are recorded and downloaded separately. Flight information can be recorded for up to 9 hours and mission information can be recorded up to 10,000 infromation packs;

    The ground monitoring and control software support online map and irregular multi- measurement automatic mapping route planning, and support automatic planning of oil, electric and other kinds of patrol, which can alert users to complete pre- flight inspection.

     

    External dimension:

    FC800: Vertical take-off and landing fixed-wing flight control and navigation system

    FC810: Tilt-rotor flight control and navigation system

    FC850: Conventional fixed-wing (hand throwing, ejection, parachute landing, sprinting take-off and

    landing) flight control and navigation system

    Features:

    The internal integrated with tri- redundancy inertia device, the main redundancy is ADI high- quality gyro and accelerometer, and can switch the standby redundancy in real time according to the working mode, with the advantages of high measurement accuracy and high reliability;

    Integrated with dual redundancy satellite navigation system, Novatel high precision real- time differential GPS module (RTK position accuracy up to centimeter) and the internal single- point positioning GPS module is redundant with each other, and the system automatically selects GPS data with better positioning status;

    Integrated with high precision dual antenna orientation module, heading measurement precision: 0.5° (0.5m baseline);

    The perfect emergency protection mechanism can protect against low voltage, low oil quantity, low speed, abnormal posture, abnormal height, low GPS position accuracy, navigation system failure, exceeding of safety and control radius ranges, remote control failure, etc.;

    It can preset 100 landing points, and automatically land nearby according to the emergency;

    Provide 8 user routes, each route can add 800 waypoints;

    It can automatically generate hovering route, hovering center, hovering radius, and number of hovering circles can be set;

    The flight information and mission information are recorded and downloaded separately. Flight information can be recorded for up to 9 hours and mission information can be recorded up to 10,000 infromation packs;

    The ground monitoring and control software support online map and irregular multi- measurement automatic mapping route planning, and support automatic planning of oil, electric and other kinds of patrol, which can alert users to complete pre- flight inspection.

     

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