📄 fdcwind.mdl
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Model {
Name "fdcwind"
Version 3.00
SimParamPage "Solver"
SampleTimeColors off
InvariantConstants off
WideVectorLines off
ShowLineWidths off
ShowPortDataTypes off
StartTime "0.0"
StopTime "50.0"
SolverMode "Auto"
Solver "ode45"
RelTol "1e-3"
AbsTol "auto"
Refine "1"
MaxStep "auto"
InitialStep "auto"
FixedStep "auto"
MaxOrder 5
OutputOption "RefineOutputTimes"
OutputTimes "[]"
LoadExternalInput off
ExternalInput "[t, u]"
SaveTime on
TimeSaveName "tout"
SaveState off
StateSaveName "xout"
SaveOutput on
OutputSaveName "yout"
LoadInitialState off
InitialState "xInitial"
SaveFinalState off
FinalStateName "xFinal"
SaveFormat "Matrix"
LimitMaxRows off
MaxRows "1000"
Decimation "1"
AlgebraicLoopMsg "warning"
MinStepSizeMsg "warning"
UnconnectedInputMsg "warning"
UnconnectedOutputMsg "warning"
UnconnectedLineMsg "warning"
InheritedTsInSrcMsg "warning"
IntegerOverflowMsg "warning"
UnnecessaryDatatypeConvMsg "none"
Int32ToFloatConvMsg "warning"
SignalLabelMismatchMsg "none"
ConsistencyChecking "off"
ZeroCross on
SimulationMode "normal"
BlockDataTips on
BlockParametersDataTip off
BlockAttributesDataTip off
BlockPortWidthsDataTip off
BlockDescriptionStringDataTip off
BlockMaskParametersDataTip off
ToolBar on
StatusBar on
BrowserShowLibraryLinks off
BrowserLookUnderMasks off
OptimizeBlockIOStorage on
BufferReuse on
BooleanDataType off
RTWSystemTargetFile "grt.tlc"
RTWInlineParameters off
RTWRetainRTWFile off
RTWTemplateMakefile "grt_default_tmf"
RTWMakeCommand "make_rtw"
RTWGenerateCodeOnly off
ExtModeMexFile "ext_comm"
ExtModeBatchMode off
ExtModeTrigType "manual"
ExtModeTrigMode "normal"
ExtModeTrigPort "1"
ExtModeTrigElement "any"
ExtModeTrigDuration 1000
ExtModeTrigHoldOff 0
ExtModeTrigDelay 0
ExtModeTrigDirection "rising"
ExtModeTrigLevel 0
ExtModeArchiveMode "off"
ExtModeAutoIncOneShot off
ExtModeIncDirWhenArm off
ExtModeAddSuffixToVar off
ExtModeWriteAllDataToWs off
ExtModeArmWhenConnect on
Created "Sat Mar 15 15:38:43 2003"
UpdateHistory "UpdateHistoryNever"
ModifiedByFormat "%<Auto>"
LastModifiedBy "campa"
ModifiedDateFormat "%<Auto>"
LastModifiedDate "Sat Feb 28 19:47:13 2004"
ModelVersionFormat "1.%<AutoIncrement:162>"
ConfigurationManager "None"
BlockDefaults {
Orientation "right"
ForegroundColor "black"
BackgroundColor "white"
DropShadow off
NamePlacement "normal"
FontName "Helvetica"
FontSize 10
FontWeight "normal"
FontAngle "normal"
ShowName on
}
AnnotationDefaults {
HorizontalAlignment "center"
VerticalAlignment "middle"
ForegroundColor "black"
BackgroundColor "white"
DropShadow off
FontName "Helvetica"
FontSize 10
FontWeight "normal"
FontAngle "normal"
}
LineDefaults {
FontName "Helvetica"
FontSize 9
FontWeight "normal"
FontAngle "normal"
}
System {
Name "fdcwind"
Location [206, 128, 697, 580]
Open on
ModelBrowserVisibility off
ModelBrowserWidth 200
ScreenColor "white"
PaperOrientation "landscape"
PaperPositionMode "auto"
PaperType "A4"
PaperUnits "centimeters"
ZoomFactor "100"
AutoZoom on
ReportName "simulink-default.rpt"
Block {
BlockType Reference
Name " F4 Phantom "
Ports [3, 3, 0, 0, 0]
Position [245, 291, 300, 409]
DropShadow on
FontName "Arial"
SourceBlock "airlib/B747"
SourceType "General Nonlinear Aircraft Model"
GM1 "[4.8768 11.79576 49.23861 33895.4489 16"
"5680.954 189543.35 0 2982.7995 0 17690.1]"
CD_wind "[0.0205 0.3 0 0 -0.1]"
CL_wind "[0.1 3.75 1.8 0 0.4]"
Cm_body "[0.025 -0.4 -2.7 0 -0.58]"
CY_body "[0 -0.68 0 0 0.0160 0.095]"
Cl_body "[0 -0.16 -0.34 0.13 -0.013 0.008]"
Cn_body "[0 0.125 -0.036 -0.270 0.001 -0.0"
"66]"
x0 "[204.7539671696894 0.0395294 -0.00488392967079 "
" 0 0 0 0 0.0395294 0 -70 -20 6065.68]"
}
Block {
BlockType Clock
Name "Clock"
Position [350, 40, 370, 60]
DisplayTime off
Decimation "10"
}
Block {
BlockType Sin
Name "Cosine"
Position [25, 60, 55, 80]
ForegroundColor "blue"
Amplitude "1"
Frequency "1"
Phase "pi/2"
SampleTime "0"
}
Block {
BlockType SubSystem
Name "F4 Rearranged"
Ports [3, 1, 0, 0, 0]
Position [245, 97, 305, 223]
DropShadow on
ShowPortLabels on
MaskDescription " The first input contains the wind velocity an"
"d acceleration.\n The second input contains external forces and moments in b"
"ody axis.\n The third input contains the deflections of elevators, ailerons,"
" rudder\n and, flaps. For a list of outputs look under the mask.\n NB : The"
" International measurement system (MKS) is adopted."
MaskPromptString "Geometry and Mass : [cbar b S Ix Iy "
" Iz Jxy Jxz Jyz m]|Aerodynamic D-Force Coefficients : [CD0 CDa CDq CDde "
"CDih]|Aerodynamic L-Force Coefficients : [CL0 CLa CLq CLde CLih]|Aerodynamic "
"Y-Moment Coefficients : [Cm0 Cma Cmq Cmde Cmih]|Aerodynamic Y-Force Coefficie"
"nts : [CY0 CYb CYp CYr CYda CYdr]|Aerodynamic X-moment Coefficients : [Cl0 Cl"
"b Clp Clr Clda Cldr]|Aerodynamic Z-moment Coefficients : [Cn0 Cnb Cnp Cnr Cnd"
"a Cndr]|Initial Condition x0 [v alpha beta p q r psi theta phi xe ye H]"
MaskStyleString "edit,edit,edit,edit,edit,edit,edit,edit"
MaskTunableValueString "on,on,on,on,on,on,on,on"
MaskCallbackString "|||||||"
MaskEnableString "on,on,on,on,on,on,on,on"
MaskVisibilityString "on,on,on,on,on,on,on,on"
MaskVariables "GM1=@1;CD_wind=@2;CL_wind=@3;Cm_body=@4;CY_body"
"=@5;Cl_body=@6;Cn_body=@7;x0=@8;"
MaskInitialization "AM=zeros(6,19);\nAM(1,[1 2 9 11 12])=reshape(CD"
"_wind,1,5);\nAM(3,[1 2 9 11 12])=reshape(CL_wind,1,5);\nAM(5,[1 2 9 11 12])=r"
"eshape(Cm_body,1,5);\nAM(2,[1 5 8 10 13 14])=reshape(CY_body,1,6);\nAM(4,[1 5"
" 8 10 13 14])=reshape(Cl_body,1,6);\nAM(6,[1 5 8 10 13 14])=reshape(Cn_body,1"
",6);\n\nIx=GM1(4);Iy=GM1(5);Iz=GM1(6);\nJxy=GM1(7);Jxz=GM1(8);Jyz=GM1(9);\n\n"
"detI = Ix*Iy*Iz - 2*Jxy*Jxz*Jyz - Ix*Jyz^2 - Iy*Jxz^2 - Iz*Jxy^2;\nI1 = Iy*"
"Iz - Jyz^2;I2 = Jxy*Iz + Jyz*Jxz;\nI3 = Jxy*Jyz + Iy*Jxz;I4 = Ix*Iz - J"
"xz^2;\nI5 = Ix*Jyz + Jxy*Jxz;I6 = Ix*Iy - Jxy^2;\n\nPl = I1/detI; Pm = I"
"2/detI; Pn = I3/detI;\nPpp = -(Jxz*I2 - Jxy*I3)/detI;Ppq = (Jxz*I1 - Jyz*I2 -"
" (Iy-Ix)*I3)/detI;\nPpr = -(Jxy*I1 + (Ix-Iz)*I2 - Jyz*I3)/detI;Pqq = (Jyz*I1 "
"- Jxy*I3)/detI;\nPqr = -((Iz-Iy)*I1 - Jxy*I2 + Jxz*I3)/detI;Prr = -(Jyz*I1 - "
"Jxz*I2)/detI;\n\nQl = I2/detI; Qm = I4/detI; Qn = I5/detI;\nQpp = -(Jxz*I4 -"
" Jxy*I5)/detI;Qpq = (Jxz*I2 - Jyz*I4 - (Iy-Ix)*I5)/detI;\nQpr = -(Jxy*I2 + (I"
"x-Iz)*I4 - Jyz*I5)/detI;Qqq = (Jyz*I2 - Jxy*I5)/detI;\nQqr = -((Iz-Iy)*I2 - J"
"xy*I4 + Jxz*I5)/detI;Qrr = -(Jyz*I2 - Jxz*I4)/detI;\n\nRl = I3/detI; Rm = I5"
"/detI; Rn = I6/detI;\nRpp = -(Jxz*I5 - Jxy*I6)/detI;\nRpq = (Jxz*I3 - Jyz*I5 "
"- (Iy-Ix)*I6)/detI;\nRpr = -(Jxy*I3 + (Ix-Iz)*I5 - Jyz*I6)/detI;\nRqq = (Jyz*"
"I3 - Jxy*I6)/detI;\nRqr = -((Iz-Iy)*I3 - Jxy*I5 + Jxz*I6)/detI;\nRrr = -(Jyz*"
"I3 - Jxz*I5)/detI;\n\nGM2 = [ Pl Pm Pn Ppp Ppq Ppr Pqq Pqr Prr ;"
"\n Ql Qm Qn Qpp Qpq Qpr Qqq Qqr Qrr ;\n "
" Rl Rm Rn Rpp Rpq Rpr Rqq Rqr Rrr ];\n\nxfix=1;"
MaskIconFrame on
MaskIconOpaque on
MaskIconRotate "none"
MaskIconUnits "autoscale"
MaskValueString "[4.8768 11.79576 49.23861 33895.4489 16"
"5680.954 189543.35 0 2982.7995 0 17690.1]|[0.0205 0.3 0 0 -0.1]"
"|[0.1 3.75 1.8 0 0.4]|[0.025 -0.4 -2.7 0 -0.58]|[0 -0."
"68 0 0 0.0160 0.095]|[0 -0.16 -0.34 0.13 -0.013 0."
"008]|[0 0.125 -0.036 -0.270 0.001 -0.066]|[204.7515252 0.03952"
"94 0 0 0 0 0 0.0395294 0 -70 -20 6065.68]"
System {
Name "F4 Rearranged"
Location [114, 249, 960, 803]
Open off
ModelBrowserVisibility off
ModelBrowserWidth 200
ScreenColor "white"
PaperOrientation "landscape"
PaperPositionMode "auto"
PaperType "usletter"
PaperUnits "inches"
ZoomFactor "100"
AutoZoom on
Block {
BlockType Inport
Name "uw,vw,ww"
Position [320, 443, 350, 457]
ForegroundColor "blue"
Port "1"
PortWidth "6"
SampleTime "-1"
DataType "auto"
SignalType "auto"
Interpolate on
}
Block {
BlockType Inport
Name "extFM"
Position [215, 168, 245, 182]
Port "2"
PortWidth "6"
SampleTime "-1"
DataType "auto"
SignalType "auto"
Interpolate on
}
Block {
BlockType Inport
Name "Deflect"
Position [80, 333, 110, 347]
Port "3"
PortWidth "-1"
SampleTime "-1"
DataType "auto"
SignalType "auto"
Interpolate on
}
Block {
BlockType SubSystem
Name "Aerodynamics"
Ports [4, 4, 0, 0, 0]
Position [190, 254, 280, 351]
FontName "Arial"
ShowPortLabels on
System {
Name "Aerodynamics"
Location [190, 638, 880, 908]
Open off
ModelBrowserVisibility off
ModelBrowserWidth 200
ScreenColor "white"
PaperOrientation "landscape"
PaperPositionMode "auto"
PaperType "usletter"
PaperUnits "inches"
ZoomFactor "100"
AutoZoom on
Block {
BlockType Inport
Name "x"
Position [45, 205, 65, 225]
DropShadow on
FontName "Arial"
Port "1"
PortWidth "-1"
SampleTime "-1"
DataType "auto"
SignalType "auto"
Interpolate on
}
Block {
BlockType Inport
Name "yad1"
Position [50, 60, 70, 80]
DropShadow on
NamePlacement "alternate"
FontName "Arial"
Port "2"
PortWidth "-1"
SampleTime "-1"
DataType "auto"
SignalType "auto"
Interpolate on
}
Block {
BlockType Inport
Name "Vw,aw,bw"
Position [45, 170, 65, 190]
DropShadow on
NamePlacement "alternate"
FontName "Arial"
Port "3"
PortWidth "3"
SampleTime "-1"
DataType "auto"
SignalType "auto"
Interpolate on
}
Block {
BlockType Inport
Name "uaero"
Position [290, 120, 310, 140]
DropShadow on
FontName "Arial"
Port "4"
PortWidth "-1"
SampleTime "-1"
DataType "auto"
SignalType "auto"
Interpolate on
}
Block {
BlockType Mux
Name "Mux3"
Ports [2, 1, 0, 0, 0]
Position [190, 162, 195, 233]
BackgroundColor "red"
ShowName off
Inputs "2"
DisplayOption "bar"
}
Block {
BlockType Selector
Name "Selector"
Position [530, 37, 575, 63]
ShowName off
Elements "[1:3]"
InputPortWidth "6"
}
Block {
BlockType Selector
Name "Selector1"
Position [530, 67, 575, 93]
ShowName off
Elements "[4:6]"
InputPortWidth "6"
}
Block {
BlockType Selector
Name "Selector2"
Position [120, 202, 170, 228]
ShowName off
Elements "[4:12]"
InputPortWidth "12"
}
Block {
BlockType SubSystem
Name "aero"
Ports [3, 1, 0, 0, 0]
Position [345, 107, 405, 153]
ShowName off
FontName "Arial"
ShowPortLabels off
MaskType "Aeromod"
MaskDescription "Aerodynamic model of the DHC-2 'Beaver'"
"."
MaskHelp "eval('fdchelp aeromod')"
MaskDisplay "disp('Aeromod\\n(General)')"
MaskIconFrame on
MaskIconOpaque on
MaskIconRotate "none"
MaskIconUnits "autoscale"
System {
Name "aero"
Location [47, 74, 789, 572]
Open off
ModelBrowserVisibility off
ModelBrowserWidth 200
ScreenColor "white"
PaperOrientation "landscape"
PaperPositionMode "auto"
PaperType "usletter"
PaperUnits "inches"
ZoomFactor "100"
AutoZoom on
Block {
BlockType Inport
Name "x"
Position [20, 80, 40, 100]
DropShadow on
FontName "Arial"
Port "1"
PortWidth "-1"
SampleTime "-1"
DataType "auto"
SignalType "auto"
Interpolate on
}
Block {
BlockType Inport
Name "uaero"
Position [20, 260, 40, 280]
DropShadow on
FontName "Arial"
Port "2"
PortWidth "-1"
SampleTime "-1"
DataType "auto"
SignalType "auto"
Interpolate on
}
Block {
BlockType Inport
Name "ydl"
Position [20, 170, 40, 190]
DropShadow on
FontName "Arial"
Port "3"
PortWidth "-1"
SampleTime "-1"
DataType "auto"
SignalType "auto"
Interpolate on
}
Block {
BlockType SubSystem
Name "0"
Ports [0, 0, 0, 0, 0]
Position [505, 15, 650, 45]
ForegroundColor "blue"
DropShadow on
ShowName off
OpenFcn "fdchelp aeromod"
FontName "Arial"
ShowPortLabels off
MaskDisplay "disp('AEROMOD\\nM.O. Rauw, October "
"1997')"
MaskIconFrame on
MaskIconOpaque on
MaskIconRotate "none"
MaskIconUnits "autoscale"
System {
Name "0"
Location [99, 72, 274, 227]
Open off
ModelBrowserVisibility off
ModelBrowserWidth 200
ScreenColor "white"
PaperOrientation "landscape"
PaperPositionMode "auto"
PaperType "usletter"
PaperUnits "inches"
ZoomFactor "100"
AutoZoom on
}
}
Block {
BlockType Demux
Name "Demux"
Ports [1, 4, 0, 0, 0]
Position [75, 52, 80, 123]
BackgroundColor "black"
ShowName off
FontName "Arial"
Outputs "[1 1 1 9]"
}
Block {
BlockType Demux
Name "Demux1"
Ports [1, 4, 0, 0, 0]
Position [75, 238, 80, 297]
BackgroundColor "black"
ShowName off
FontName "Arial"
Outputs "4"
}
Block {
BlockType Fcn
Name "Fcn"
Position [215, 70, 255, 90]
ShowName off
FontName "Arial"
Expr "u[1]^2"
}
Block {
BlockType Fcn
Name "Fcn1"
Position [215, 90, 255, 110]
ShowName off
FontName "Arial"
Expr "u[1]^3"
}
Block {
BlockType Fcn
Name "Fcn2"
Position [215, 130, 255, 150]
ShowName off
FontName "Arial"
Expr "u[1]^2"
}
Block {
BlockType Fcn
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