基于Matlab实现风力涡轮机系统模型仿真（源码+数据+说明文档）.rar

removed variables: ------------------------------------------------------------------------------------------------------------------------------------ 9999.9 TiDynBrk - Time to initiate deployment of the dynamic generator brake [CURRENTLY IGNORED] (s) 1 PSpnElN - Number of the innermost blade element which is still part of the pitchable portion of the blade for partial-span pitch control [1 to BldNodes] [CURRENTLY IGNORED] (-) DynBrkFi - File containing a mech-gen-torque vs HSS-speed curve for a dynamic brake [CURRENTLY IGNORED] (quoted string) False CalcTMode - Calculate tower mode shapes internally {T: ignore mode shapes from below, F: use mode shapes from below} [CURRENTLY IGNORED] (flag) False CalcBMode - Calculate blade mode shapes internally {T: ignore mode shapes from below, F: use mode shapes from below} [CURRENTLY IGNORED] (flag) "NRELOffshrBsline5MW_Platform_Monopile_RF.dat" PtfmFile - Name of file containing platform properties (quoted string) [unused when PtfmModel=0] False Platform - Read in additional data for platform (flag) 3 ADAMSPrep - ADAMS preprocessor mode {1: Run FAST, 2: use FAST as a preprocessor to create an ADAMS model, 3: do both} (switch) 1 AnalMode - Analysis mode {1: Run a time-marching simulation, 2: create a periodic linearized model} (switch) "NRELOffshrBsline5MW_ADAMSSpecific.dat" ADAMSFile - Name of file containing ADAMS-specific input parameters (quoted string) [unused when ADAMSPrep=1] "NRELOffshrBsline5MW_Linear.dat" LinFile - Name of file containing FAST linearization parameters (quoted string) [unused when AnalMode=1] NoiseFile - Name of file containing aerodynamic noise input parameters (quoted string) [used only when CompNoise=True] False CompNoise - Compute aerodynamic noise (flag) PtfmLdMod is now CompUserPtfmLd TwrLdMod is now CompUserTwrLd %BJJ ==> Check bugzilla bug 195 variables still to be removed: ------------------------------------------------------------------------------------------------------------------------------------ ADAMS columns in Tower and Blade files removed (keep code for now) AeroCent column in blade file removed... look for repurcussions... should be in AeroDyn ---------------------- TIP-BRAKE ----------------------------------------------- 0.0 TBDrConN - Tip-brake drag constant during normal operation, Cd*Area (m^2) 0.0 TBDrConD - Tip-brake drag constant during fully-deployed operation, Cd*Area (m^2) 0.0 TpBrDT - Time for tip-brake to reach full deployment once released (sec) 9999.9 TTpBrDp(1) - Time to initiate deployment of tip brake 1 (s) 9999.9 TTpBrDp(2) - Time to initiate deployment of tip brake 2 (s) 9999.9 TTpBrDp(3) - Time to initiate deployment of tip brake 3 (s) [unused for 2 blades] 9999.9 TBDepISp(1) - Deployment-initiation speed for the tip brake on blade 1 (rpm) 9999.9 TBDepISp(2) - Deployment-initiation speed for the tip brake on blade 2 (rpm) 9999.9 TBDepISp(3) - Deployment-initiation speed for the tip brake on blade 3 (rpm) [unused for 2 blades] tip-brake aerodynamics: let's not support it in this version furling: let's not support it in this version adams: let's not support it in this version controls: add simple yaw control: fixed yaw with this variable: 0.0 YawNeut - Neutral yaw position--yaw spring force is zero at this yaw (degrees) <--- RENAME THIS VARIABLE ed: Outputs that are invalid now: ! RotCq -> uses airdensity ! RotCp -> uses airdensity ! RotCt -> uses airdensity ! HSShftCq -> uses airdensity ! HSShftCp -> uses airdensity ! GenCq -> uses airdensity ! GenCp -> uses airdensity ! NacYawErr -> only computed with CompAero.... is this a SrvD output now? HSSBrTq GenTq GenPwr WindVxi WindVyi WindVzi TotWindV HorWindV HorWndDir VerWndDir TFinAlpha TFinCLift TFinCDrag TFinDnPrs TFinCPFx TFinCPFy