UC5_TC_14Preconditions: 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).https://repo.valu3s.eu/use-cases/aircraft-engine-controller/test-cases/uc5_tc_14https://repo.valu3s.eu/@@site-logo/logo_valu3s_green_transparent.png
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).