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adding new section in wrong spot
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@gbarter
gbarter committed Mar 3, 2022
1 parent 9e32fb7 commit ec6d5ae
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Showing 2 changed files with 10 additions and 10 deletions.
10 changes: 5 additions & 5 deletions OpenFAST/IEA-15-240-RWT-Monopile/IEA-15-240-RWT-Monopile_ServoDyn.dat
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Original file line number Diff line number Diff line change
Expand Up @@ -48,11 +48,6 @@ True GenTiStp - Method to stop the generator {T: timed usin
9999.9 THSSBrDp - Time to initiate deployment of the HSS brake (s)
9999.9 HSSBrDT - Time for HSS-brake to reach full deployment once initiated (sec) [used only when HSSBrMode=1]
9999.9 HSSBrTqF - Fully deployed HSS-brake torque (N-m)
---------------------- Aerodynamic Flow Control -------------------------------------
0 AfCmode - Airfoil control mode {0- none, 1- cosine wave cycle, 4- user-defined from Simulink/Labview, 5- user-defined from Bladed-style DLL}
0.0 AfC_Mean - Mean level for sinusoidal cycling or steady value (-) [used only with AfCmode==1]
0.0 AfC_Amp - Amplitude for for cosine cycling of flap signal (AfC = AfC_Amp*cos(Azimuth+phase)+AfC_mean) (-) [used only with AfCmode==1]
0.0 AfC_phase - Phase relative to the blade azimuth (0 is vertical) for for cosine cycling of flap signal (deg) [used only with AfCmode==1]
---------------------- NACELLE-YAW CONTROL -------------------------------------
0 YCMode - Yaw control mode {0: none, 3: user-defined from routine UserYawCont, 4: user-defined from Simulink/Labview, 5: user-defined from Bladed-style DLL} (switch)
9999.9 TYCOn - Time to enable active yaw control (s) [unused when YCMode=0]
Expand All @@ -62,6 +57,11 @@ True GenTiStp - Method to stop the generator {T: timed usin
9999.9 TYawManS - Time to start override yaw maneuver and end standard yaw control (s)
0.25 YawManRat - Yaw maneuver rate (in absolute value) (deg/s)
0.0 NacYawF - Final yaw angle for override yaw maneuvers (degrees)
---------------------- Aerodynamic Flow Control -------------------------------------
0 AfCmode - Airfoil control mode {0- none, 1- cosine wave cycle, 4- user-defined from Simulink/Labview, 5- user-defined from Bladed-style DLL}
0.0 AfC_Mean - Mean level for sinusoidal cycling or steady value (-) [used only with AfCmode==1]
0.0 AfC_Amp - Amplitude for for cosine cycling of flap signal (AfC = AfC_Amp*cos(Azimuth+phase)+AfC_mean) (-) [used only with AfCmode==1]
0.0 AfC_phase - Phase relative to the blade azimuth (0 is vertical) for for cosine cycling of flap signal (deg) [used only with AfCmode==1]
---------------------- STRUCTURAL CONTROL ---------------------------------------
0 NumBStC - Number of blade structural controllers (integer)
"unused" BStCfiles - Name of the file for blade tuned mass damper (quoted string) [unused when CompNTMD is false]
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10 changes: 5 additions & 5 deletions ...EA-15-240-RWT-Monopile_wDTUcontroller/IEA-15-240-RWT-Monopile_ServoDyn_wDTUcontroller.dat
View file
Original file line number Diff line number Diff line change
Expand Up @@ -48,11 +48,6 @@ True GenTiStp - Method to stop the generator {T: timed usin
9999.9 THSSBrDp - Time to initiate deployment of the HSS brake (s)
9999.9 HSSBrDT - Time for HSS-brake to reach full deployment once initiated (sec) [used only when HSSBrMode=1]
9999.9 HSSBrTqF - Fully deployed HSS-brake torque (N-m)
---------------------- Aerodynamic Flow Control -------------------------------------
0 AfCmode - Airfoil control mode {0- none, 1- cosine wave cycle, 4- user-defined from Simulink/Labview, 5- user-defined from Bladed-style DLL}
0.0 AfC_Mean - Mean level for sinusoidal cycling or steady value (-) [used only with AfCmode==1]
0.0 AfC_Amp - Amplitude for for cosine cycling of flap signal (AfC = AfC_Amp*cos(Azimuth+phase)+AfC_mean) (-) [used only with AfCmode==1]
0.0 AfC_phase - Phase relative to the blade azimuth (0 is vertical) for for cosine cycling of flap signal (deg) [used only with AfCmode==1]
---------------------- NACELLE-YAW CONTROL -------------------------------------
0 YCMode - Yaw control mode {0: none, 3: user-defined from routine UserYawCont, 4: user-defined from Simulink/Labview, 5: user-defined from Bladed-style DLL} (switch)
9999.9 TYCOn - Time to enable active yaw control (s) [unused when YCMode=0]
Expand All @@ -62,6 +57,11 @@ True GenTiStp - Method to stop the generator {T: timed usin
9999.9 TYawManS - Time to start override yaw maneuver and end standard yaw control (s)
0.25 YawManRat - Yaw maneuver rate (in absolute value) (deg/s)
0.0 NacYawF - Final yaw angle for override yaw maneuvers (degrees)
---------------------- Aerodynamic Flow Control -------------------------------------
0 AfCmode - Airfoil control mode {0- none, 1- cosine wave cycle, 4- user-defined from Simulink/Labview, 5- user-defined from Bladed-style DLL}
0.0 AfC_Mean - Mean level for sinusoidal cycling or steady value (-) [used only with AfCmode==1]
0.0 AfC_Amp - Amplitude for for cosine cycling of flap signal (AfC = AfC_Amp*cos(Azimuth+phase)+AfC_mean) (-) [used only with AfCmode==1]
0.0 AfC_phase - Phase relative to the blade azimuth (0 is vertical) for for cosine cycling of flap signal (deg) [used only with AfCmode==1]
---------------------- STRUCTURAL CONTROL ---------------------------------------
0 NumBStC - Number of blade structural controllers (integer)
"unused" BStCfiles - Name of the file for blade tuned mass damper (quoted string) [unused when CompNTMD is false]
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