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Flight Control and Navigation Computer
A Series Flight Control:
A3
A4
A5
B Series Flight Control:
B2
B4
B7
B8
E Series Flight Control:
E1
M Series Flight Control:
Ultra-Micro Flight Control
XF Series Flight Control:
XF10
XF20
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Semi-physical simulation experimental system based on OBS
Ground station equipment
Avionics equipment
Simulation equipment
A4 series flight control and navigation computer: suitable for small, electric, fixed-wing, tiltorotor, quadcopter, and other aircraft.
B7 series flight control and navigation computer: suitable for all quadcopters.
XF20 is a standard autonomous vehicle: supports GNSS guidance and cockpit guidance, suitable for fixed-wing aircraft, multiple task routes.
SESRVICE & SUPPORT
Design and Simulation Service
Software Development Service
Hardware Development Service
Integration Testing Service
Flight Testing Service
Typical Case - Fixed Wing
Typical Case - Vertical Take-off and Landing
Typical Case - Multiple-copter
Typical Case - Special Application
Typical Case - Patrol guidance
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Flight Control and Navigation Computer
XF Series flight control - XF10
XF Series flight control - XF10
XF10 is the basic autopilot, suitable for conventional layout, flying wing, V-tail fixed wing aircraft, using GNSS guidance.
Innovation Creation Specialties Focus
Demand driven UAV navigation guidance and control system servicer.
Product Features
Suitable for conventional layout, flying wing, V-tail fixed wing aircraft.
Minimal pre-shooting preparation, solidified launch process, zero-base operation, support mobile APP control, to meet the needs of fast response.
Using GNSS guidance mode, two-point straight flight from launch point to target point.
Supports only ground speed flight, reducing airspeed calibration.
With GNSS signal loss protection, timeout without connection can control aircraft self-destruct, function can be disabled.
Electronic fence and no-fly zone can be customized, aircraft self-destruct can be controlled, function can be disabled.
No flight data recording function to ensure information security.
Low voltage, remote control signal loss, radio loss can continue to perform the task, no return event.
Configurable launch mode.
Configurable power and rudder starting logic.
With control parameter binding function.
Integrated GNSS/IMU navigation.
External magnetometer, support magnetic compass pre-installation calibration; navigation has self-alignment function, supports moving base alignment.
Survive by quality, develop by reputation, and continue to create value for customers
Performance Parameters
System Performance
Attitude Accuracy RMS
1°
Heading Accuracy RMS
2°
Single Point Positioning Accuracy
2.5m
Single Point Velocity Accuracy
0.1m/s
Altitude Measurement Range
<18000m
Servomechanism/Motor Update Frequency
≤500Hz
Servomechanism Power Supply
Current ≤3A, unlimited voltage
External Interface
TTL
3
SBUS
1
PWM
8
IO
1
AD
2
Electrical Parameter
Supply Voltage
DC5±0.5V
Power Consumption
<1W
Physical Parameter
Dimension
85.14mm×45mm×18mm
Weight
60.5g
Environmental Parameter
Operating Temperature
-20℃~55℃
Storage Temperature
-40℃~85℃