UC5_TC_14

Preconditions: Aircraft is in operating mode M; Input conditions / steps: Observed aircraft thrust is at value V1, small perturbations in non-pilot input cause it to change to V2, and outside air pressure abruptly changes from P1 to P2; Expected results: Observed aircraft thrust returns to value V1, respecting control objectives (settling time, overshoot, steady state error).
14
Safety
Aircraft Engine + Controller (Model, Software)
VALU3S Framework
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