FC400 Flight Control
Performance index:
|
Parameter |
index |
|
Attitude precision |
0.5° |
|
Heading precision |
2° |
|
Position accuracy |
2.5m |
|
Angular velocity measurement range |
±500° /s |
|
Acceleration measurement range |
±4g |
|
Height measuring range |
-500m ～ 10000m |
|
The range of voltage monitoring |
0 ～ 52V |
|
Servo updating frequency |
50Hz |
|
Engine speed monitoring range |
0 ～ 20000RPM |
|
Communication interface |
RS- 232C |
|
Voltage monitoring |
2 channels |
|
Engine speed monitoring range |
2 channels |
|
PWM control range |
9 channels |
|
Digital output range |
3 channels（PWM programmable） |
|
Expansion serial port |
3 channels（connect RTK, mission payload, etc.） |
|
Sbus input range |
1 channel |
|
Number of routes |
8 routes（800 waypoints on each route） |
|
Built-in data logger |
9 hours |
|
Photographing point |
10000 points |
|
Emergency landing point |
100 points |
|
Electrical parameters |
|
|
Power supply voltage |
DC4.5- 9.0V |
|
Power consumption |
＜ 3W |
|
Physical parameters |
|
|
Weight |
≤130 g |
|
Dimensions（mm） |
109*56*29.5 |
|
Environment parameters |
|
|
Working temperature |
-20℃～ 55℃ |
|
Storage temperature |
-40℃～ 85℃ |
FC400: Electric vertical take-off and landing fixed-wing flight control and navigation system
FC410: Electric tilt-rotor flight control and navigation system
FC450: Electric conventional fixed-wing (hand throwing, ejection, parachute landing) flight control and navigation system
Support 4 forms of UAVs (including conventional tail, V- tail, and flying wings) electric and oil- powered composite (vertical take- off and landing fixed- wing), conventional fixed- wing, tilt- rotor and multi- rotor;
Integrated with micro GPS/MINS integrated navigation system, barometric altimeter, differential pressure, airspeed meter, 2- channel speed measurement, 1- channel oil quantity measurement;
Support external differential GPS (RTK, PPK, Dual antenna directional function are all optional), and the external differential GPS is redundant with internal single- point GPS module, and the system will automatically select the better one;
Support external compass, which is convenient for users to select the area with less magnetic interference to improve the heading measurement accuracy;
Support automatic ignition function after the UAV drived by oil take- off;
The perfect emergency protection mechanism can protect against low voltage, low oil quantity, low speed, abnormal posture, high altitude, 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 near the emergency protection;
Provide 8 user routes, each route can add 800 waypoints; automatically generate hovering route, hovering center, hovering radius, and number of hovering circles can be set;
Provide photo (shutter control) function in the flight segment and also timing/fixed- distance setting can be set;
Support typical photoelectric pods, open platform, and three- axis platform control for special rotation and control of surveying and mapping;
The flight and mission information are recorded and downed separately. The flight information recording time is up to 9 hours, and the mission information record can reach 10,000 information 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 patrol routes, which can alert users to complete pre- flight inspection.
