[tabs][tab title=”Introduction”]AIC built-in sensing unit integrated six-degrees of freedom inertial MENS sensor(MENS IMU), 3-axis magnetic compass, and a high sensitivity GNSS (GPS & GLONASS) receiver. Combined with the precise GPS assisted correcting to achieve the IMU to perform the high accuracy navigation flight control.

Data processing by UKF algorithm ensures accuracy, stability and fast convergence AHRS information for well execution of high accuracy attitude and heading flight control.

            

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Basic architecture diagram

The system of flight control mainly includes four modules as follows,

a)AHRS module

b)FCC module

c)Data storage module

d)GPS & Compass module

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The specification of AXH-E230 with AXC-10 autopilot flight control

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