FC800 Flight Control
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℃ |
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.