FC700 Flight Control
Performance index:
|
Parameter |
index |
|
Attitude accuracy |
0.1° (GNSS valid) |
|
Course accuracy |
0.1° (2m baseline) |
|
RTK positioning accuracy |
5cm+1ppm |
|
Velocity accuracy |
0.1m/s |
|
Gyroscope measurement range |
±500° /s |
|
Accelerometer measurement range |
±8g |
|
Height measuring range |
- 500m ～ 10000m |
|
Voltage monitoring range |
0 ～ 52V |
|
Steering gear update frequency |
50Hz ～ 200Hz |
|
Engine speed monitoring range |
0 ～ 20000RPM |
|
Voltage monitoring channel |
2 channels |
|
Engine speed monitoring channel |
2 channels |
|
PWM control channel |
9 channels |
|
Digital output channel |
3 channels（PWM programmable） |
|
CAN communication interface |
1 channels |
|
Composite navigation output interface |
2 channels |
|
Guide output interface |
1 channels |
|
Second pulse signal |
1 channels |
|
Sbus interface |
1 channels input, 1 channels output |
|
Extended serial port |
4 channels RS232 |
|
Electrical parameters |
|
|
Power supply voltage |
DC4.5- 9.0V |
|
Power consumption |
＜ 3W |
|
Physical parameters |
|
|
Weight |
≤160 g |
|
Dimensions（mm） |
109*56*30.7 |
|
Environment parameters |
|
|
Working temperature |
-40℃～ 85℃ |
|
Storage temperature |
-40℃～ 85℃ |
FC700: Vertical Takeoff and Landing Fixed wing Flight Control and Navigation system
FC710: Conventional fixed-wing flight control and navigation system for skidding Take-off and landing
Integrated high precision multi-redundancy IMUs, dynamic attitude accuracy 0.1°, principal and redundancy of high precision gyroscope and accelerometer, and can be real according to the working state ;
It has the advantages of high measurement accuracy and high reliability.
Integrated high-precision dual antenna directional system, course accuracy 0.1° (2m baseline), and double redundant magnetic compass system together to form a three-redundant heading system.
Greatly improve the reliability of navigation system;
Integrated high-precision BD/GPS real-time differential positioning module, the guide frequency supports 20Hz, support dynamic differential positioning;
12 PWM control output, 4 serial port output, 2 ADC input, 2 speed monitoring, 1 CAN, 1 SBUS input, 1 Route SBUS output;
Support the direct output of guide and integrated navigation original data, can be synchronized second pulse signal;
Support flight control formation simulation in the loop (flight control embedded digital aircraft model);
Support shipborne takeoff and landing, networking formation, terminal guidance and other functions, support user customization;
Support fixed-wing, vertical takeoff and landing fixed-wing, multi-rotor models;
Perfect emergency protection mechanism, can prevent low power, low oil, low speed, attitude abnormal, altitude abnormal, GPS positioning accuracy low, navigation system fault, Beyond the safety fence, beyond the control radius, remote control failure and other protection;
100 emergency landing points can be preset to automatically land nearby in case of emergency protection;
10 flight routes, including 8 mission routes, each mission route can reach up to 800 navigation points;
Automatically generate circling route, circling center, circling radius, circling circle number can be set;
Flight information and mission information are recorded and downloaded separately. The flight information recording time is up to 9 hours, and the mission information recording time can reach 10,000 pieces.
Ground measurement and control software supports online map and irregular multi-survey area automatic mapping route planning, support oil, electric power lines such as automatic route planning, can Alert the user for a complete pre-flight check.
