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A8 Flight control computer (highly reliable, dual core) for medium electric, oil-powered fixed-wing, vertical take-off and landing aircraft of 100 kg and above.
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A Series flight control - A4
The A4 series flight control and navigation computer is suitable for small electric, oil-operated fixed wing, vertical take-off and landing, tilt-rotor, multicopter and other aircraft. Internal integration of GNSS/SINS integrated navigation,, redundant IMU configuration with built-in calibrated shock absorber, using J30 connector to improve system reliability.
Innovation
Creation
Specialities
Focus
Demand driven UAV navigation guidance and control system servicer
Product features
- Suitable for small electric, oil powered fixed wing, vertical take-off and landing, tilt-rotor, multicopter and other aircraft.
- Internal integration of maximum 60km P840 digital radio, GNSS/INS integrated navigation,air pressure altimeter, airspeed meter, magnetic compass and other sensors, redundant IMU configuration, and built-in calibrated shock absorber.
- Support external differential GNSS with RTK and dual antenna orientation to improve positioning and orientation accuracy, and redundancy with internal GNSS module.
- Support external magnetic compass, easy to install in areas with less magnetic interference.
- Support for automatic ignition control of the piston.
- Fully autonomous flight control function.
- Complete emergency protection mechanism, including low voltage, GNSS signal loss, remote control failure protection, etc. Electronic fence and emergency landing point can be set.
- Support autonomous photo control, ground station can be configured to support photoelectric pod, open Pan&Tilt, servo Pan&Tilt control, support 10 routes, 1000 waypoints per route.
- Built-in data logger, support more than 10h data storage, support cyclic storage.
- Ground station software supports online map, automatic route planning for non-regular areas,pre-flight check warning and in-flight warning functions.
Survive by quality,
develop by reputation,
and continue to create value for customers
develop by reputation,
and continue to create value for customers
Performance parameters
System performance
Attitude accuracy RMS
1°
Heading accuracy RMS
2°
Dual Antenna Orientation Accuracy RMS
0.1°(1m baseline)
Single point positioning accuracy 1σ
2.5m
Single point velocity accuracy 1σ
0.1m/s
RTK positioning accuracy 1σ
0.8cm+1ppm(Level)
1.5cm+1ppm(elevation)
Altitude measurement range
<18000m
Number of routes
10 (1000 waypoints for each)
Data logging
10h cyclic storage
Servo/motor update frequency
≤500Hz
External interface
TTL
2
RS232
1
CAN
1
SBUS
1(Input)、1(output)
PWM
8
Analogue
2
Digital
1(Multiplexable to PWM)
5V power supply
2(Limited to 0.3A)
Electrical parameters
Supply voltage
DC4.5~12V
Power dissipation
＜3.5W
Physical parameters
Dimension
123mm×75mm×36mm
Weight
263g
Environmental parameters
Operating temperature
-20℃~55℃
Storage temperature
-40℃~85℃
