tm_icl.524.0

多学科优化软件isight培训教程初级pdf有很详细的例子讲解

api_StartTask ACSanalysis

api_SetVersionInfo ACSanalysis \
   -mdolVersion 6.0

api_SetCompileOptions ACSanalysis \
   -errorLevel warn \
   -topologyFile {}

api_SetBlockComments ACSanalysis \
   Optimization PriorityRankedPlan { PLAN TO BE CONFIGURED BY ADVISOR:}

api_SetTaskHeader ACSanalysis \
   -description {
      ""
   } \
   -version 1.0 \
   -color Gray \
   -directorySearchList {
   } \
   -evaluation {taskplan} \
   -controlMode user \
   -userMode interactive \
   -precision double \
   -elapseTime 259200 \
   -runCounter 1 \
   -autoPath {
   } \
   -auditEnable {
   } \
   -auditDisable {
   } \
   -checkPoint unknown \
   -boundsPolicy adjustbound \
   -randGenInit default \
   -switchOn {
   } \
   -switchOff {
   }

api_SetInputs ACSanalysis \
   -parameters {
      {WingArea 135.0 REAL unknown ""}
      {FuseLength 20.0 REAL unknown ""}
      {CruiseVel 200.0 REAL unknown ""}
      {WtFuel 139.2 REAL unknown ""}
      {AR 5.6 REAL unknown ""}
      {CLmax 1.92 REAL unknown ""}
      {sfc 1.816e-07 REAL unknown ""}
      {PropEfficiency 0.945 REAL unknown ""}
      {UltLoadFactor 4.56 REAL unknown ""}
      {WtEng 141.84 REAL unknown ""}
      {WtPayload 286.56 REAL unknown ""}
      {FuseDia 4.05 REAL unknown ""}
      {density 0.0021 REAL unknown ""}
      {NumPass 2 INTEGER unknown ""}
      {NumEng 1 INTEGER unknown ""}
      {AircraftRangeRequired 565.0 REAL unknown ""}
      {VstallMax 70.0 REAL unknown ""}
   }

api_SetAuxiliaries ACSanalysis \
   -parameters {
   }

api_SetOutputs ACSanalysis \
   -parameters {
      {WetArea REAL "%s" ""}
      {LoD REAL "%s" ""}
      {EmptyWeight REAL "%s" ""}
      {TotalWeight REAL "%s" ""}
      {AircraftRange REAL "%s" ""}
      {StallSpd REAL "%s" ""}
      {ObjectiveWeight REAL "%s" ""}
      {AircraftRangeConstraint REAL "%s" ""}
      {StallConstraint REAL "%s" ""}
      {Objective REAL "%s" ""}
      {Feasibility INTEGER "%s" ""}
      {TaskProcessStatus REAL "%s" ""}
   }

api_SetGroup ACSanalysis OutputConstraintsGroup \
   { AircraftRangeConstraint StallConstraint }

api_SetGroup ACSanalysis InputConstraintsGroup \
   { PropEfficiency NumPass WtFuel WingArea CruiseVel AR density FuseLength FuseDia NumEng }

api_SetGroup ACSanalysis VariablesGroup \
   { AR WingArea FuseLength FuseDia density CruiseVel WtFuel NumPass NumEng WtEng WtPayload UltLoadFactor PropEfficiency sfc CLmax AircraftRangeRequired VstallMax }

api_SetGroup ACSanalysis OutputsGroup \
   { WetArea LoD EmptyWeight TotalWeight AircraftRange StallSpd ObjectiveWeight AircraftRangeConstraint StallConstraint }

api_SetGroup ACSanalysis AuxiliariesGroup \
   { }

api_SetGroup ACSanalysis InputsGroup \
   { WingArea FuseLength CruiseVel WtFuel AR CLmax sfc PropEfficiency UltLoadFactor WtEng WtPayload FuseDia density NumPass NumEng AircraftRangeRequired VstallMax }

api_SetInitialization ACSanalysis \
   -parameters {
   } \
   -expressions {
   }

api_SetCalculation ACSanalysis Evaluation \
   -parameters {
      TotalWeight
      AircraftRange
      AircraftRangeRequired
      StallSpd
      VstallMax
      ObjectiveWeight
      AircraftRangeConstraint
      StallConstraint
   } \
   -expressions {
set ObjectiveWeight(V) [expr $TotalWeight(V)]
set AircraftRangeConstraint(V) [expr $AircraftRange(V)/$AircraftRangeRequired(V)-1.0]
set StallConstraint(V) [expr 1.0-$StallSpd(V)/$VstallMax(V)]
}

   api_StartSimcode AircraftSizing
      api_SetStandardInputFile farFile0 \
         -simcode AircraftSizing \
         -templateFile "ACSInTemp.dat" \
         -inputFile "ACSIn.txt" \
         -nameValueFile "MDOLGEN_ACSanalysis.1" \
         -translationFile "MDOLGEN_ACSanalysis.2" \
         -saveTranslationFile no \
         -parameters {
            AR
            WingArea
            FuseLength
            FuseDia
            density
            CruiseVel
            WtFuel
            NumPass
            NumEng
            WtEng
            UltLoadFactor
            WtPayload
            PropEfficiency
            sfc
            CLmax
            AircraftRangeRequired
            VstallMax
         } \
         -instructions { 
find "'AR'" 
replace word with $AR
find "'Swing'" 
replace word with $WingArea
find "'Lfuse'" 
replace word with $FuseLength
find "'Dfuse'" 
replace word with $FuseDia
find "'rho'" 
replace word with $density
find "'vel'" 
replace word with $CruiseVel
find "'Wfuel'" 
replace word with $WtFuel
find "'Npass'" 
replace word with $NumPass
find "'Nen'" 
replace word with $NumEng
find "'Wen'" 
replace word with $WtEng
find "'Wpay'" 
replace word with $WtPayload
find "'Nzult'" 
replace word with $UltLoadFactor
find "'eta'" 
replace word with $PropEfficiency
find "'c'" 
replace word with $sfc
find "'clmax'" 
replace word with $CLmax
find "'reqrange'" 
replace word with $AircraftRangeRequired
find "'VstallMax'" 
replace word with $VstallMax
 }

      api_SetStandardOutputFile farFile1 \
         -simcode AircraftSizing \
         -outputFile "ACSOut.txt" \
         -nameValueFile "MDOLGEN_ACSanalysis.3" \
         -translationFile "MDOLGEN_ACSanalysis.4" \
         -saveTranslationFile no \
         -parameters {
            WetArea
            LoD
            EmptyWeight
            TotalWeight
            AircraftRange
            StallSpd
         } \
         -instructions { 
find "1" 
read WetArea
provide $WetArea 
find "2" 
read LoD
provide $LoD
find "3" 
read EmptyWeight
provide $EmptyWeight
find "4" 
read TotalWeight
provide $TotalWeight
find "5" 
read AircraftRange
provide $AircraftRange
find "6" 
read StallSpd
provide $StallSpd
 }

   api_SetSimcode AircraftSizing \
      -program "../Programs/acs.exe" \
      -processType transient \
      -elapseTime 20 \
      -prolog {
         {WriteInputFiles farFile0}
      } \
      -epilog {
         {ReadOutputFiles farFile1}
      } \
      -executionTemplate {$Program}

   api_EndSimcode AircraftSizing


api_StartProcess ACSanalysis
api_SetTaskProcess ACSanalysis \
   -prolog {
   } \
   -epilog {
      {ScaleConstraints}
      {CalculateObjective}
      {PostEvent TaskProcessCompleted}
   } \
   -controlParameters {
   } \
   -control {
      {EvaluateSimcode AircraftSizing}
      {EvaluateCalculation Evaluation}
   }

api_EndProcess ACSanalysis


api_SetDataStorage ACSanalysis \
   -restore no \
   -dataLog {"doe.db" overwrite on {
      }
   } \
   -dataLookUp {on {
         "doe.db"
      }
   } \
   -matchMode Exact \
   -matchTolerance {} \
   -levels { 0 1 2 3 4 5 6 7 8 9 } \
   -storeGrad yes \
   -storeApprox yes \
   -condition {} \
   -parameters {
   }

api_StartOptimization ACSanalysis
api_SetOptimizationPlan ACSanalysis PriorityRankedPlan \
   -prolog {
   } \
   -epilog {
   } \
   -description {} \
   -defaultUpperBound 1E15 \
   -useScaling yes \
   -terminationCriteria { \
   } \
   -variables {
      AR
      WingArea
      FuseLength
      FuseDia
      CruiseVel
      WtFuel
      WtEng
      WtPayload
      UltLoadFactor
      PropEfficiency
      sfc
      CLmax
   } \
   -potentialVariables {
      AR
      WingArea
      FuseLength
      FuseDia
      density
      CruiseVel
      WtFuel
      NumPass
      NumEng
      WtEng
      WtPayload
      UltLoadFactor
      PropEfficiency
      sfc
      CLmax
      AircraftRangeRequired
      VstallMax
   } \
   -variableScaling {
      {AR 1.0}
      {WingArea 1.0}
      {FuseLength 1.0}
      {FuseDia 1.0}
      {density 1.0}
      {CruiseVel 1.0}
      {WtFuel 1.0}
      {NumPass 1.0}
      {NumEng 1.0}
      {WtEng 1.0}
      {WtPayload 1.0}
      {UltLoadFactor 1.0}
      {PropEfficiency 1.0}
      {sfc 1.0}
      {CLmax 1.0}
      {AircraftRangeRequired 1.0}
      {VstallMax 1.0}
   } \
   -inputConstraints {
      {PropEfficiency lower 0.5}
      {PropEfficiency upper 1.18125}
      {NumPass lower 1}
      {NumPass upper 8}
      {WtFuel lower 100}
      {WtFuel upper 2000}
      {WingArea lower 100}
      {WingArea upper 300}
      {CruiseVel lower 150.0}
      {CruiseVel upper 312.5}
      {AR lower 4.2}
      {AR upper 9}
      {density lower 1.9e-3}
      {density upper 2.378e-3}
      {FuseLength lower 15.0}
      {FuseLength upper 31.25}
      {FuseDia lower -20}
      {FuseDia upper 20}
      {NumEng lower 1}
      {NumEng upper 4}
   } \
   -potentialObjectives {
      WetArea
      LoD
      EmptyWeight
      TotalWeight
      AircraftRange
      StallSpd
      ObjectiveWeight
      AircraftRangeConstraint
      StallConstraint
   } \
   -objectives {
      {ObjectiveWeight minimize 1.0 1.0}
   } \
   -outputConstraints {
      {AircraftRangeConstraint lower 0 1.0 1.0}
      {StallConstraint lower 0 1.0 1.0}
      {TaskProcessStatus upper 0.0 1.0 1.0}
   } \
   -controlParameters {
   } \
   -control {
   }

api_EndOptimization ACSanalysis


api_SetTaskPlan ACSanalysis \
   -prologue {
   } \
   -epilogue {
   } \
   -controlParameters {
   } \
   -control {
      {EvaluateOptimizePlan PriorityRankedPlan}
   }

api_SetCheckPoint ACSanalysis \
   -files {
   } \
   -save {
   } \
   -restore {
   }

api_SetTaskCleanup ACSanalysis \
   -parameters {
   } \
   -expressions {
   } \
   -deleteFiles {
      "MDOLGEN_ACSanalysis.1"
      "MDOLGEN_ACSanalysis.2"
      "MDOLGEN_ACSanalysis.3"
      "MDOLGEN_ACSanalysis.4"
   }

api_SetProcedures ACSanalysis \
   -tclSourceFiles {
   } \
   -procedures {
   }

api_EndTask ACSanalysis