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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 - A8
The A8 series flight control and navigation computer is positioned as a professional grade, highly reliable product, suitable for medium-sized electric, oil-powered fixed-wing, vertical take-off and landing aircraft of 100 kg and above, with a dual redundant MCU , internal integration of triple-redundant IMU , the main IMU is ADI high-quality gyro and adder,integrated high precision compass, atmospheric data system, built-in GPS and Novatel high-precision differential GNSS module, internal reinforcement design and shock-resistant storage, with better environmental adaptability.
Innovation
Creation
Specialities
Focus
Demand driven UAV navigation guidance and control system servicer
Product features
- Suitable for medium-sized electric, oil-operated fixed-wing and vertical take-off and landing aircraft of 100 kg and above.
- Temperature control measures and reinforcement measures, with a wide temperature range of -40℃~85℃ and vibration and shock resistance.
- Dual redundancy MCU, which greatly enhances system safety and reliability.
- Internal integration of GNSS/IMU integrated navigation, triple redundant IMU, ADI high quality gyro and adder for main IMU.
- Integrated total pressure, static pressure and total temperature sensors, with professional atmospheric data system.
- Integrated single-point GNSS and Novatel high-precision differential GNSS modules, with RTK and dual-antenna orientation functions to improve positioning and orientation accuracy, and redundant GNSS modules.
- Supports external magnetic compass for easy installation in areas with low magnet.
- Support for external navigation system.
- Equipped with shock-resistant storage function, which can be used as a black box.
- Equipped with RS422 communication chip, supports RS422 interface communication externally.
- Fully autonomous flight control function.
- Support automatic ignition control of fuel plane.
- 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 and 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
0.5°
Heading accuracy RMS
1.5°
Dual Antenna Orientation Accuracy RMS
0.1°(1m baseline)
Single point positioning accuracy 1σ
1m
Single point velocity accuracy 1σ
0.1m/s
RTK positioning accuracy 1σ
1cm+1ppm
Altitude measurement range
<18000m
Number of routes
10 (1000 waypoints for each)
Data logging
10h cyclic storage
Servo/motor update frequency
50Hz~200Hz
External interface
TTL
1+1 Optional
RS232
1
RS422/485
2
CAN
2
SBUS
1(Input)、1(output)
PWM
12
Analogue
6
Digital
3(Multiplexable to PWM)
5V power supply
2(Limited to 0.3A)
Electrical parameters
Supply voltage
DC9~36V
Power dissipation
＜6W
Physical parameters
Dimension
138mm×100mm×47mm
Weight
379g
Environmental parameters
Operating temperature
-40℃~85℃
Storage temperature
-40℃~85℃
