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FC800 Flight Control

FC800 Flight Control

Model: FC800

Short Description:

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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Technical Parameter

External dimension

Features

Product Tags

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 channelsPWM programmable

Expansion serial port

3 channelsconnect 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

Dimensionsmm

153*98*47.5

Environment parameters

Working temperature

-40℃85℃

Storage temperature

-40℃85℃


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  • 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

    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.