The S40 (cost- effective), flight control and navigation system, is designed for small size conventional fixed- wing, vertical take- off and landing fixed- wing, tilt - rotor aircraft, with integrated flight control computer and micro- integrated navigation system (GPS/MINS).
Product Description
The S40 (cost- effective), flight control and navigation system, is designed for small size conventional fixed- wing, vertical take- off and landing fixed- wing, tilt - rotor aircraft, with integrated flight control computer and micro- integrated navigation system (GPS/MINS). It is capable for one- key action, enabling automatic take- off and landing, hovering, circling, returning, altitude holding, parachute landing and various forms of autonomous cruise function according to the setting route. It provides a comprehensive flight status monitoring, alarm function and a comprehensive emergency protection mechanism to ensure the safe operation of the system.
System performance index
Attitude precision
1°
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
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 suppty voltage
DC4.5 - 9.0V
Power consumption
< 4W
Physical parameters
Weight
130g
Dimensions (mm)
108*56*29.5
Environment parameters
Working temperature
- 20℃ - 55℃
Storage temperature
- 40℃ - 85℃