function [stateUpd,finalAlpha,alphaList,diff,SysDataUpd,SysParaUpd,maps]=... simulationCutMotorInstant(busTag,SysData,SysDataBase,SysPara,SimData,maps,x0,indCutIdx) % Simulate cut induction motor % % FUNCTION simulationCutMotorInstant % % Author: Rui Yao % % Copyright (C) 2021, UChicago Argonne, LLC. All rights reserved. % % OPEN SOURCE LICENSE % % Redistribution and use in source and binary forms, with or without modification, are permitted provided that the following conditions are met: % % 1. Redistributions of source code must retain the above copyright notice, this list of conditions and the following disclaimer. % 2. Redistributions in binary form must reproduce the above copyright notice, this list of conditions and the following disclaimer in the documentation and/or other materials provided with the distribution. % 3. Neither the name of the copyright holder nor the names of its contributors may be used to endorse or promote products derived from this software without specific prior written permission. % % % ****************************************************************************************************** % DISCLAIMER % % THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS "AS IS" AND ANY EXPRESS OR IMPLIED % WARRANTIES, INCLUDING, BUT NOT LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS FOR A % PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE COPYRIGHT HOLDER OR CONTRIBUTORS BE LIABLE FOR ANY % DIRECT, INDIRECT, INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, BUT NOT LIMITED TO, % PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER % CAUSED AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR % OTHERWISE) ARISING IN ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE POSSIBILITY OF SUCH DAMAGE. % *************************************************************************************************** % % INPUT % busTag - Tags for determining the partial system that will be kept % SysData - System data for simulation % SysDataBase - Base system data for simulation % SysPara - Parameters representing the events happening in the system % SimData - Simulation parameters % *Map - The mapping of current data to base data % inv*Map - Inverse mapping, base data to current data % x0 - Initial system state % indCutIdx - Index of cut motor % % OUTPUT % stateNew - Solved new state % finalAlpha - The ending alpha % alphaList - A list of alphas % diff - Equation mismatches % SysDataUpd - Updated system data % *Map - The mapping of current data to base data (updated) % inv*Map - Inverse mapping, base data to current data (updated) % [bus,sw,pv,pq,shunt,line,ind,zip,syn,exc,tg,agc,cac,cluster]=unfoldSysData(SysData); [busBase,swBase,pvBase,pqBase,shuntBase,lineBase,indBase,zipBase,synBase,excBase,tgBase,agcBase,cacBase,clusterBase]=unfoldSysData(SysDataBase); [~,~,~,~,~,~,~,~,~,~,~,~,~,~,~,~,~,~,~,~,~,~,fault]=unfoldSysPara(SysPara); busMap=maps.busMap;invBusMap=maps.invBusMap; indMap=maps.indMap;invIndMap=maps.invIndMap; synMap=maps.synMap;invSynMap=maps.invSynMap; lineMap=maps.lineMap;invLineMap=maps.invLineMap; [~,~,~,~,~,~,~,~,method]=unfoldSimData(SimData); AEmethod=round(10*mod(method,1)); pqIncrS=zeros(size(pq,1),2);pvIncrS=zeros(size(pv,1),1); nbus=size(bus,1); nZip=size(zip,1); nInd=size(ind,1); Rzip0S=ones(nZip,1);Rzip1S=zeros(nZip,1); Rind0S=ones(nInd,1);Rind1S=zeros(nInd,1); [~,Ytr0,Ysh0,~,~,~,~]=getYMatrix(nbus,line,fault); newIndIdx=indMap(indCutIdx); activeNewIndCutIdx=newIndIdx(newIndIdx~=0); indTag=zeros(size(ind,1),1); indTag(activeNewIndCutIdx)=1; [V,Q,s,d,w,eq1,eq2,ed1,ed2,psid,psiq,Pm,Ef,Vavrm,Vavrr,Vavrf,Vavrref,tgovg,tgovm,tgovmech,f,dpg,qplt,vg]=unfoldX(x0,SysData); s0Cut=s(indTag==1); activeIndRemainIdx=find(indTag==0); invActiveIndRemainIdx=zeros(nInd,1); invActiveIndRemainIdx(activeIndRemainIdx)=1:length(activeIndRemainIdx); Z1=ind(activeNewIndCutIdx,7)+1j*ind(activeNewIndCutIdx,8); Ze=1j*ind(activeNewIndCutIdx,13); R2=ind(activeNewIndCutIdx,9); X2=ind(activeNewIndCutIdx,10); Zind0=Z1+Ze.*(R2+1j*X2.*s0Cut)./(R2+(Ze+1j*X2).*s0Cut); % Only valid for 3rd order model Yind0=1./Zind0; Ysh1=-accumarray(ind(activeNewIndCutIdx,1),Yind0,[nbus,1]); Ysh0=Ysh0-Ysh1; ind=ind(activeIndRemainIdx,:); Rind0S=Rind0S(activeIndRemainIdx); Rind1S=Rind1S(activeIndRemainIdx); SysDataUpd=foldSysData(bus,sw,pv,pq,shunt,line,ind,zip,syn,exc,tg,agc,cac,cluster); s=s(activeIndRemainIdx); x0=foldX(SysDataUpd,V,Q,s,d,w,eq1,eq2,ed1,ed2,psid,psiq,Pm,Ef,Vavrm,Vavrr,Vavrf,Vavrref,tgovg,tgovm,tgovmech,f,dpg,qplt,vg); indMap(invIndMap)=invActiveIndRemainIdx; invIndMap=invIndMap(activeIndRemainIdx); SysParaSim=foldSysPara(pqIncrS,pvIncrS,Rind0S,Rind1S,[],[],Rzip0S,Rzip1S,Ytr0,0*Ytr0,Ysh0,Ysh1,[],[],[],[],[]); if ~isempty(busTag)&&~isempty(find(busTag==0,1)) % Purge system with busTag [SysDataUpdFtr,busFtr,swFtr,pvFtr,pqFtr,shuntFtr,lineFtr,indFtr,zipFtr,synFtr,excFtr,tgFtr,... busMap,indMap,synMap,lineMap,invBusMap,invIndMap,invSynMap,invLineMap]=... filterSysData(busTag,SysDataUpd,busMap,indMap,synMap,lineMap,invBusMap,invIndMap,invSynMap,invLineMap); SysParaSim=filterSysPara(SysParaSim,busFtr,swFtr,pvFtr,pqFtr,shuntFtr,lineFtr,indFtr,zipFtr,synFtr,excFtr,tgFtr); SysPara=filterSysPara(SysPara,busFtr,swFtr,pvFtr,pqFtr,shuntFtr,lineFtr,indFtr,zipFtr,synFtr,excFtr,tgFtr); x0=filterX(SysDataUpd,SysDataUpdFtr,x0,busFtr,swFtr,pvFtr,pqFtr,shuntFtr,lineFtr,indFtr,zipFtr,synFtr,excFtr,tgFtr); SysDataUpd=SysDataUpdFtr; end xNew=x0; if AEmethod==0 [stateNew,finalAlpha,alphaList,diff]=solveAlgebraicHem(SimData,SysDataUpd,SysParaSim,x0,xNew); else [stateNew,flag,diff,loop]=solveAlgebraicNR(SimData,SysDataUpd,SysParaSim,x0,xNew); if flag==0 finalAlpha=1; else finalAlpha=0; end alphaList=linspace(0,finalAlpha,loop); end stateUpd=stateNew; SysParaUpd=SysPara; maps.busMap=busMap;maps.invBusMap=invBusMap; maps.indMap=indMap;maps.invIndMap=invIndMap; maps.synMap=synMap;maps.invSynMap=invSynMap; maps.lineMap=lineMap;maps.invLineMap=invLineMap; end