a is developed, and protection level calculations for the angle-of-attack a and sideslip ß are derived. A simulation is presented to showcase the air data fault detection and isolation algorithm. Specifically, the impact of the external disturbance, the motion of the dynamics and the airspeed fault on a and ß state errors, and the detection capability are discussed. Furthermore, the protection levels of a and ß are illustrated.">

A Fault Detection and Isolation Design for a Dual Pitot Tube Air Data System (original) (raw)

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