fast_advance_states()
- ed_updatestates
- SolveOption2a_Inp2BD 
	- ed_calc_output 更新数据

- BD updatestates
- SolveOption2b_Inp2IfW Ifw根据ED结果更新

- ifw updatestates
- SolveOption2c_Inp2AD_SrvD 
	- ifw calcoutput 
	- AD_InputSolve_IfW
	- SrvD_InputSolve
		- ``! from Ifw``
		- WindDir
		- HorWindV
		- LidSpeed
		- MsrPositionsX
		- MsrPositionsY
		- MsrPositionsZ
		- 
		- ``! from ED``
		- YawAngle
		- Yaw
		- YawRate
		- LSS_Spd
		- HSS_Spd
		- RotSpeed
		- RootMxc
		- RootMyc
		- YawBrTAxp
		- YawBrTAyp
		- LSSTipPxa
		- LSSTipMxa
		- LSSTipMya
		- LSSTipMza
		- LSSTipMys
		- LSSTipMzs
		- YawBrMyn
		- YawBrMzn
		- NcIMURAxs
		- NcIMURAys
		- NcIMURAzs
		- RotPwr
		- LSShftFxa
		- LSShftFys
		- LSShftFzs

- SrvD_UpdateStates
	- SrvD_CopyInput
	- SrvD_Input_ExtrapInterp
	- SrvD_UpdateDiscState
	- SrvD_Input_ExtrapInterp
	- DLL_controller_call
	- Torque_UpdateStates
	- Pitch_UpdateStates
	- Yaw_UpdateStates
	- TipBrake_UpdateStates
	
	- ! Blade Nacelle Tower Platform StrucCtrl，但是NumSStC = 0 这部分代码跳过
	- ! Compute ElecPwr and GenTrq for controller (and DLL needs this saved):
		- CalculateTorque

CalcOutputs_And_SolveForInputs
- SolveOption2 
	- AD_CalcOutput
	- SrvD_CalcOutput
	- ED_InputSolve  ED接收AD SD输入
		- BladeLoads.force/moment
		- towerloads.force/moment
		
		- GenTrq
		- HSSBrTrqC
		- BlPitchCom
		- YawMom
		- StrucCtrl loads 暂时没有
		
		-  NacelleLoads.force/moment

- Transfer_SrvD_to_SD_MD

- ! 都在ifw更新后 
- SrvD_InputSolve

- ResetRemapFlags

ed 到Bladed dll的输出：

```
   y%RotPwr    = m%AllOuts(  RotPwr)*1000.
   DO K=1,p%NumBl
      y%RootMxc(K)   = m%AllOuts( RootMxc(K) )*1000.
      y%RootMyc(K)   = m%AllOuts( RootMyc(K) )*1000.
   END DO
   y%YawBrTAxp = m%AllOuts( YawBrTAxp)
   y%YawBrTAyp = m%AllOuts( YawBrTAyp)
   !y%LSSTipPxa = m%AllOuts( LSSTipPxa)*D2R ! bjj: did this above already

   y%LSSTipMxa = m%AllOuts(LSShftMxa)*1000.
   y%LSSTipMya = m%AllOuts(LSSTipMya)*1000.                ! Rotating hub My (GL co-ords) (Nm)
   y%LSSTipMza = m%AllOuts(LSSTipMza)*1000.                ! Rotating hub Mz (GL co-ords) (Nm)
   y%LSSTipMys = m%AllOuts(LSSTipMys)*1000.                ! Fixed hub My (GL co-ords) (Nm)
   y%LSSTipMzs = m%AllOuts(LSSTipMzs)*1000.                ! Fixed hub Mz (GL co-ords) (Nm)
   y%YawBrMyn  = m%AllOuts( YawBrMyn)*1000.                ! Yaw bearing My (GL co-ords) (Nm) !tower accel
   y%YawBrMzn  = m%AllOuts( YawBrMzn)*1000.                ! Yaw bearing Mz (GL co-ords) (Nm)
   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
   y%NcIMURAys = m%AllOuts(NcIMURAys)*D2R                  ! Nacelle nodding acceleration (rad/s^2)
   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
   y%LSShftFxa = m%AllOuts(LSShftFxa)*1000.                ! Rotating low-speed shaft force x (GL co-ords) (N)
   y%LSShftFys = m%AllOuts(LSShftFys)*1000.                ! Nonrotating low-speed shaft force y (GL co-ords) (N)
   y%LSShftFzs = m%AllOuts(LSShftFzs)*1000.                ! Nonrotating low-speed shaft force z (GL co-ords) (N)
```

```
 m%AllOuts(LSShftMxa) =  DOT_PRODUCT( MomLPRot, m%CoordSys%e1 )
 m%AllOuts(   RotPwr) = ( x%QDT(DOF_GeAz) + x%QDT(DOF_DrTr) )*m%AllOuts(LSShftMxa)
 
DO K=1,p%NumBl
	m%AllOuts( RootMxc(K) ) = DOT_PRODUCT( MomH0B(:,K), m%CoordSys%i1(K,:) )
	m%AllOuts( RootMyc(K) ) = DOT_PRODUCT( MomH0B(:,K), m%CoordSys%i2(K,:) )
END DO !K

m%AllOuts(YawBrTAxp) =  DOT_PRODUCT( LinAccEO, m%CoordSys%b1 )
m%AllOuts(YawBrTAyp) = -DOT_PRODUCT( LinAccEO, m%CoordSys%b3 )

y%LSSTipPxa = x%QT (DOF_GeAz) + x%QT  (DOF_DrTr) + p%AzimB1Up + PiBy2
m%AllOuts(LSSTipPxa) = y%LSSTipPxa*R2D


m%AllOuts(LSShftMxa) =  DOT_PRODUCT( MomLPRot, m%CoordSys%e1 )
m%AllOuts(LSSTipMya) =  DOT_PRODUCT( MomLPRot, m%CoordSys%e2 )
m%AllOuts(LSSTipMza) =  DOT_PRODUCT( MomLPRot, m%CoordSys%e3 )
m%AllOuts(LSSTipMys) = -DOT_PRODUCT( MomLPRot, m%CoordSys%c3 )
m%AllOuts(LSSTipMzs) =  DOT_PRODUCT( MomLPRot, m%CoordSys%c2 )

m%AllOuts( YawBrMyn) = -DOT_PRODUCT( MomBNcRt, m%CoordSys%d3 )
m%AllOuts( YawBrMzn) =  DOT_PRODUCT( MomBNcRt, m%CoordSys%d2 )


m%AllOuts(NcIMURAxs) =      DOT_PRODUCT(                 AngAccER  , m%CoordSys%c1 )*R2D
m%AllOuts(NcIMURAys) = -1.0*DOT_PRODUCT(                 AngAccER  , m%CoordSys%c3 )*R2D
m%AllOuts(NcIMURAzs) =      DOT_PRODUCT(                 AngAccER  , m%CoordSys%c2 )*R2D

m%AllOuts(LSShftFxa) =  DOT_PRODUCT(  FrcPRot, m%CoordSys%e1 )
m%AllOuts(LSShftFys) = -DOT_PRODUCT(  FrcPRot, m%CoordSys%c3 )
m%AllOuts(LSShftFzs) =  DOT_PRODUCT(  FrcPRot, m%CoordSys%c2 )
```