A Fault Detection and Localization of An Helicopter Execution Element

Abstract

Before a system can attempt to deal with a fault, one must first make an assessment of its location. Increasing of an exception indicates the presence of a fault, and in many systems no further information is available to assist fault location. In this case, automatic repair of the system will only be possible if the exception provides an accurate guide to the location of the fault. Like an example a fuzzy FDI system for an execution element of a helicopter is illustrated.