UC5_TC_15

Preconditions: Aircraft is in operating mode M; Input conditions / steps: Observed aircraft thrust is at value V1, pilot input changes from A1 to A2, and outside air pressure abruptly changes from P1 to P2; Expected results: Observed aircraft thrust changes and settles to value V2, respecting operating limit objectives (e.g., upper limit in shaft speed).
15
Safety
Aircraft Engine + Controller (Model, Software)
VALU3S Framework
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