| 摘要 |
An avionic aviation system ( 80 ) and corresponding method with ground station ( 81 ) for automatic elimination of resulting failures in aircraft ( 40/41/42 ) are proposed. The avionic aviation system ( 80 ) is linked to a multiplicity of aircraft ( 40/41/42 ) via a wireless interface ( 402 ) of the avionics ( 403 ). If a failure is detected in an aircraft ( 40, . . . , 42 ) by means of a sensor ( 3/401/601 ), a dedicated failure deployment device ( 603 ) for automatic failure elimination is selected by means of a filter module ( 2 ) and a switching device ( 1 ) of the ground station ( 81 ) for activation of the failure deployment device ( 603 ) is specifically enabled.
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