| 摘要 |
The present invention provides a method for providing a fault diagnosis for at least one system, in particular of an aircraft. The method comprises: (a) providing a number N1, n1epsilon[1, . . . , N1], of systems, wherein the n1-th system, in each case, provides a number N2, n2epsilon[1, . . . , N2], of instances of a main function of a number N3, n3epsilon[1, . . . , N3], of main functions of the aircraft; (b) providing a number N4, n4epsilon[1, . . . , N4], of IMA modules, wherein in each case the n4-th IMA module provides resources at least for the respective n2-th instances of the main functions; (c) providing a generic diagnostic unit; (d) instantiating the generic diagnostic unit to provide a predetermined number N5, n5epsilon[1, . . . , N5], of instances of the generic diagnostic unit; and (e) configuring the n5-th instance, in each case, of the generic diagnostic unit for adaption of the corresponding n5-th diagnostic unit to at least one system.
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