Test bench development for the functional hazards assesment of an integrated flight control system validation using model-based design
Integrated flight control system of a civil aircraft safety requirements validation process using means of model-based design is considered. The necessity for correct Functional Hazard Assessment is explained. Hardware and software needed for the problem are described. Complex mathematical model structure and human machine interface are provided.
Key words: model-based design, control systems, flight safety, requirements validation.
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