FIELD: aviation; aeronautics.
SUBSTANCE: invention relates to automated detection of structural damages. Integrated system for assessment of state and control of a structural platform in flight includes a structural integrity control system (SHM) and a workload control system (OLM) connected to sensors of the SHM system. OLM system comprises a processor which, when the structural platform is in flight, applies parametric models using flight parameter data, to assess actual use of structural components by analyzing static characteristics, fatigue characteristics and damage resistance (FDTA), using parametric models and finite element model results. In the data bank, a maintenance plan is stored, containing inspection periods and tasks of the structural platform. Subsystem for evaluation of detected structural damages (iSRM) generates warnings to pilot during flight upon detection of damage.
EFFECT: broader functional capabilities.
11 cl, 5 dwg
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