UC5_TC_11

Preconditions: Aircraft is in operating mode M and system parameter P deviates at most +/- R % from nominal value; Input conditions / steps: Observed aircraft thrust is at value V1 and pilot input changes from A1 to A2; Expected results: Observed aircraft thrust changes and settles to value V2, respecting operating limit objectives (e.g., upper limit in shaft speed).
11
Safety
Aircraft Engine + Controller (Model, Software)
VALU3S Framework
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