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The flight control laws design process
We propose and apply a structured design process for flight control laws. This process is based on object-oriented modelling technology, advanced and/or classical controller synthesis methods, multi-objective parameter synthesis, and efficient analysis methods for performance and robustness assessment. The process supports handling of complex controller structures, addressing of the full envelope of aircraft loading and operating conditions, handling of large amounts of multi-disciplinary design criteria, and handling of various types of uncertainty and parameter variation.
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