149 lines
4.7 KiB
Markdown
149 lines
4.7 KiB
Markdown
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fast_advance_states()
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- ed_updatestates
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- SolveOption2a_Inp2BD
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- ed_calc_output 更新数据
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- BD updatestates
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- SolveOption2b_Inp2IfW Ifw根据ED结果更新
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- ifw updatestates
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- SolveOption2c_Inp2AD_SrvD
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- ifw calcoutput
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- AD_InputSolve_IfW
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- SrvD_InputSolve
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- ``! from Ifw``
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- WindDir
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- HorWindV
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- LidSpeed
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- MsrPositionsX
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- MsrPositionsY
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- MsrPositionsZ
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-
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- ``! from ED``
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- YawAngle
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- Yaw
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- YawRate
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- LSS_Spd
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- HSS_Spd
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- RotSpeed
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- RootMxc
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- RootMyc
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- YawBrTAxp
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- YawBrTAyp
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- LSSTipPxa
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- LSSTipMxa
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- LSSTipMya
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- LSSTipMza
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- LSSTipMys
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- LSSTipMzs
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- YawBrMyn
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- YawBrMzn
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- NcIMURAxs
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- NcIMURAys
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- NcIMURAzs
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- RotPwr
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- LSShftFxa
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- LSShftFys
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- LSShftFzs
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- SrvD_UpdateStates
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- SrvD_CopyInput
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- SrvD_Input_ExtrapInterp
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- SrvD_UpdateDiscState
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- SrvD_Input_ExtrapInterp
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- DLL_controller_call
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- Torque_UpdateStates
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- Pitch_UpdateStates
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- Yaw_UpdateStates
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- TipBrake_UpdateStates
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- ! Blade Nacelle Tower Platform StrucCtrl，但是NumSStC = 0 这部分代码跳过
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- ! Compute ElecPwr and GenTrq for controller (and DLL needs this saved):
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- CalculateTorque
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CalcOutputs_And_SolveForInputs
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- SolveOption2
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- AD_CalcOutput
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- SrvD_CalcOutput
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- ED_InputSolve ED接收AD SD输入
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- BladeLoads.force/moment
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- towerloads.force/moment
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- GenTrq
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- HSSBrTrqC
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- BlPitchCom
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- YawMom
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- StrucCtrl loads 暂时没有
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- NacelleLoads.force/moment
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- Transfer_SrvD_to_SD_MD
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- ! 都在ifw更新后
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- SrvD_InputSolve
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- ResetRemapFlags
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ed 到Bladed dll的输出：
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```
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y%RotPwr = m%AllOuts( RotPwr)*1000.
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DO K=1,p%NumBl
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y%RootMxc(K) = m%AllOuts( RootMxc(K) )*1000.
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y%RootMyc(K) = m%AllOuts( RootMyc(K) )*1000.
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END DO
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y%YawBrTAxp = m%AllOuts( YawBrTAxp)
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y%YawBrTAyp = m%AllOuts( YawBrTAyp)
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!y%LSSTipPxa = m%AllOuts( LSSTipPxa)*D2R ! bjj: did this above already
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y%LSSTipMxa = m%AllOuts(LSShftMxa)*1000.
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y%LSSTipMya = m%AllOuts(LSSTipMya)*1000. ! Rotating hub My (GL co-ords) (Nm)
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y%LSSTipMza = m%AllOuts(LSSTipMza)*1000. ! Rotating hub Mz (GL co-ords) (Nm)
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y%LSSTipMys = m%AllOuts(LSSTipMys)*1000. ! Fixed hub My (GL co-ords) (Nm)
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y%LSSTipMzs = m%AllOuts(LSSTipMzs)*1000. ! Fixed hub Mz (GL co-ords) (Nm)
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y%YawBrMyn = m%AllOuts( YawBrMyn)*1000. ! Yaw bearing My (GL co-ords) (Nm) !tower accel
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y%YawBrMzn = m%AllOuts( YawBrMzn)*1000. ! Yaw bearing Mz (GL co-ords) (Nm)
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y%NcIMURAxs = m%AllOuts(NcIMURAxs)*D2R ! Nacelle roll acceleration (rad/s^2) -- this is in the shaft (tilted) coordinate system, instead of the nacelle (nontilted) coordinate system
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y%NcIMURAys = m%AllOuts(NcIMURAys)*D2R ! Nacelle nodding acceleration (rad/s^2)
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y%NcIMURAzs = m%AllOuts(NcIMURAzs)*D2R ! Nacelle yaw acceleration (rad/s^2) -- this is in the shaft (tilted) coordinate system, instead of the nacelle (nontilted) coordinate system
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y%LSShftFxa = m%AllOuts(LSShftFxa)*1000. ! Rotating low-speed shaft force x (GL co-ords) (N)
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y%LSShftFys = m%AllOuts(LSShftFys)*1000. ! Nonrotating low-speed shaft force y (GL co-ords) (N)
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y%LSShftFzs = m%AllOuts(LSShftFzs)*1000. ! Nonrotating low-speed shaft force z (GL co-ords) (N)
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```
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```
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m%AllOuts(LSShftMxa) = DOT_PRODUCT( MomLPRot, m%CoordSys%e1 )
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m%AllOuts( RotPwr) = ( x%QDT(DOF_GeAz) + x%QDT(DOF_DrTr) )*m%AllOuts(LSShftMxa)
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DO K=1,p%NumBl
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m%AllOuts( RootMxc(K) ) = DOT_PRODUCT( MomH0B(:,K), m%CoordSys%i1(K,:) )
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m%AllOuts( RootMyc(K) ) = DOT_PRODUCT( MomH0B(:,K), m%CoordSys%i2(K,:) )
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END DO !K
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m%AllOuts(YawBrTAxp) = DOT_PRODUCT( LinAccEO, m%CoordSys%b1 )
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m%AllOuts(YawBrTAyp) = -DOT_PRODUCT( LinAccEO, m%CoordSys%b3 )
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y%LSSTipPxa = x%QT (DOF_GeAz) + x%QT (DOF_DrTr) + p%AzimB1Up + PiBy2
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m%AllOuts(LSSTipPxa) = y%LSSTipPxa*R2D
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m%AllOuts(LSShftMxa) = DOT_PRODUCT( MomLPRot, m%CoordSys%e1 )
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m%AllOuts(LSSTipMya) = DOT_PRODUCT( MomLPRot, m%CoordSys%e2 )
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m%AllOuts(LSSTipMza) = DOT_PRODUCT( MomLPRot, m%CoordSys%e3 )
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m%AllOuts(LSSTipMys) = -DOT_PRODUCT( MomLPRot, m%CoordSys%c3 )
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m%AllOuts(LSSTipMzs) = DOT_PRODUCT( MomLPRot, m%CoordSys%c2 )
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m%AllOuts( YawBrMyn) = -DOT_PRODUCT( MomBNcRt, m%CoordSys%d3 )
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m%AllOuts( YawBrMzn) = DOT_PRODUCT( MomBNcRt, m%CoordSys%d2 )
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m%AllOuts(NcIMURAxs) = DOT_PRODUCT( AngAccER , m%CoordSys%c1 )*R2D
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m%AllOuts(NcIMURAys) = -1.0*DOT_PRODUCT( AngAccER , m%CoordSys%c3 )*R2D
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m%AllOuts(NcIMURAzs) = DOT_PRODUCT( AngAccER , m%CoordSys%c2 )*R2D
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m%AllOuts(LSShftFxa) = DOT_PRODUCT( FrcPRot, m%CoordSys%e1 )
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m%AllOuts(LSShftFys) = -DOT_PRODUCT( FrcPRot, m%CoordSys%c3 )
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m%AllOuts(LSShftFzs) = DOT_PRODUCT( FrcPRot, m%CoordSys%c2 )
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``` |