code.ans.desc

多学科优化软件isight培训教程初级pdf有很详细的例子讲解

MDOLVersion: 6.0
CompilerOptions: warn

Task Airplane

    TaskHeader Airplane
        Version: 1.0
        Evaluation: single
        ControlMode: user
        RunCounter: 1
        BoundsPolicy: adjustvalue
        CheckPoint: unknown
    End TaskHeader Airplane

    Inputs Airplane
        Parameter: WingSpan Type: real InitialValue: 22.72
        Parameter: WingArea Type: real InitialValue: 117.3
        Parameter: FuseLength Type: real InitialValue: 32.6
        Parameter: FuseDia Type: real InitialValue: 4.85
    End Inputs Airplane

    Outputs Airplane
        Parameter: SurfAreaFuse Type: real
        Parameter: WetArea Type: real
        Parameter: LoD Type: real
    End Outputs Airplane

    SimCode AeroCode
        InputFiles AeroCode
            FileDescription AeroIntxt
                FileType: standard
                TemplateFile: "AeroInTemp.dat"
                InputFile: "AeroIn.txt"
                Parameters
                    WingSpan WingArea FuseLength FuseDia
                Instructions
                    find "b     = " ignore 
                    write $WingSpan as "%7.3f"
                    find "Swing = " ignore 
                    replace word with $WingArea 
                    find "Lfuse = " ignore 
                    replace word with $FuseLength 
                    find "Dfuse = " ignore 
                    replace word with $FuseDia as "%9.5f"
                End Instructions
            End FileDescription AeroIntxt
        End InputFiles AeroCode

        OutputFiles AeroCode
            FileDescription AeroOuttxt
                FileType: standard
                OutputFile: "AeroOut.txt"
                Parameters
                    SurfAreaFuse WetArea LoD
                Instructions
                    find "Surface Area of the Fuselage = " ignore 
                    read SurfAreaFuse as "%g"
                    provide $SurfAreaFuse 
                    find "Wetted Area of the Aircraft  = " ignore 
                    read WetArea as "%g"
                    provide $WetArea 
                    find "Lift/Drag of the Aircraft    = " ignore 
                    read LoD as "%g"
                    provide $LoD
                End Instructions
            End FileDescription AeroOuttxt
        End OutputFiles AeroCode

        SimCodeProcess AeroCode
            Program: "../Programs/aero.exe"
            ElapseTime: 5m
            Prologue
                WriteInputSpecs: AeroIntxt
            Epilogue
                ReadOutputSpecs: AeroOuttxt
            Execution: "$Program"
        End SimCodeProcess AeroCode

    End SimCode AeroCode

    TaskProcess Airplane
        Control: [
            AeroCode
        ]
    End TaskProcess Airplane

    Optimization Airplane
        PotentialVariables:
            WingSpan WingArea FuseLength FuseDia
        Variables:
            WingSpan WingArea FuseLength FuseDia
        VariableScaling
            Parameter: WingSpan ScaleFactor: 1.0
            Parameter: WingArea ScaleFactor: 1.0
            Parameter: FuseLength ScaleFactor: 1.0
            Parameter: FuseDia ScaleFactor: 1.0
        PotentialObjectives:
            WingSpan WingArea FuseLength FuseDia SurfAreaFuse WetArea LoD

        # PLAN TO BE CONFIGURED BY ADVISOR:
        OptimizePlan PriorityRankedPlan
            Control: [
            ]
    End Optimization Airplane

    TaskPlan Airplane
        Control: [
            PriorityRankedPlan
        ]
    End TaskPlan Airplane

    DataStorage Airplane
        Restore: no
        DataLog: "code.ans.db" Mode: overwrite
        DataLookUp: "Airplane.db"
        MatchMode: Exact
        Levels: all
        StoreGradRuns: yes
        StoreApproxRuns: yes
    End DataStorage Airplane

End Task Airplane