Invention Grant
US08346408B2 Fault tolerant flight control system 有权
容错飞行控制系统

Fault tolerant flight control system
Abstract:
A method, apparatus, and computer program product for identifying a number of air states for a vehicle. A deflection of a control surface associated with an actuator is identified to form an identified deflection. A current in the actuator is identified to form a measured current. The number of air states for the vehicle is estimated using the identified deflection and the measured current.
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