Dual Redundant Flight Computer

ADASI FC-200 Flight Computer

Dual Redundant Flight Computer

Two independent processing boards interfaced with a redundant, shared interface controller. 

Two independent power supply units

Internal encrypted data storage 

Two internal IMUs 

Two internal GNSS receivers  

Built-in test and redundancy for reliable and safe operation 

Dual redundant arbitration function for master processor board selection  

Multiple interface options for sensors, control surfaces, lift motors, power plant and various other avionics sub-systems.