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A4系列飞行控制与导航计算机:适用于小型电动、油动固定翼、倾转旋翼、多旋翼等飞行器
B7系列飞行控制与导航计算机:适用于各类多旋翼飞行器
XF20 is an indicator autopilot: GNSS guidance and pod guidance C methods, types of fixed wing, various types of mission routes
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A Series flight control - A7
The A7 series flight control and navigation computer is suitable for medium to large electric, oil powered fixed wing, vertical take-off and landing, tilt-rotor, multicopper and other aircraft. It integrates three redundant IMU inertial devices internally, and the main IMU uses ADI high-quality gyroscope and accelerometer, integrating total pressure, static pressure, and total temperature sensors. It is equipped with a professional atmospheric data system, GPS+RTK, and supports optional built-in radios. It has a richer external interface and is a professional, high-performance, high integration, and cost-effective flight control and navigation equipment.
Innovation
Creation
Specialities
Focus
Demand driven UAV navigation guidance and control system servicer
Product features
- Suitable for medium to large electric, oil moving fixed wing, vertical takeoff and landing, tiltrotor, multi rotor and other aircraft.
- Temperature control measures, with a wide temperature range of -40℃~55℃.
- 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.
- Internal integration of single-point GNSS and differential GNSS, with RTK and dual-antenna orientation functions to improve positioning and orientation accuracy, and redundant GNSS modules.
- Support for external magnetic compass, easy to install in areas with low magnetic interference.
- Support for external navigation system.
- 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
0.75°
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
50Hz~200Hz
External interface
TTL
1+1 Optional
RS232
2
RS422/485
2
CAN
2
SBUS
1(Input)、1(output)
PWM
12
AD
6
IO
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×32mm
Weight
333g
Environmental parameters
Operating temperature
-40℃~55℃
Storage temperature
-55℃~85℃
