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powersas.m/internal/simulationAddMotorInstant.m

132 lines
6.2 KiB

function [stateUpd,finalAlpha,alphaList,diff,SysDataUpd,SysParaUpd,maps]=...
simulationAddMotorInstant(busTag,SysData,SysDataBase,SysPara,SimData,maps,x0,indAddIdx,TmAdd,s0Add)
% Simulate add induction motor
%
% FUNCTION simulationAddMotorInstant
%
% Author: Rui Yao <ruiyao@ieee.org>
%
% 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
% indAddIdx - Index of added motor
% TmAdd - Instant torque of the added motor
% s0Add - Instant slip of the added 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);
indAdd=indBase(indAddIdx,:);
indAdd(~isnan(TmAdd),15)=TmAdd(~isnan(TmAdd));
indAdd(~isnan(TmAdd),[16,17])=0;
indAdd(:,1)=busMap(indAdd(:,1));
ind=[ind;indAdd];
indMap(indAddIdx)=(size(invIndMap,1)+1):(size(invIndMap,1)+length(indAddIdx));
invIndMap=[invIndMap;indAddIdx];
Z1=indAdd(:,7)+1j*indAdd(:,8);
Ze=1j*indAdd(:,13);
R2=indAdd(:,9);
X2=indAdd(:,10);
Zind0=Z1+Ze.*(R2+1j*X2.*s0Add)./(R2+(Ze+1j*X2).*s0Add);
Yind0=1./Zind0;
Ysh1=accumarray(indAdd(:,1),Yind0,[nbus,1]);
SysParaSim=foldSysPara(pqIncrS,pvIncrS,Rind0S,Rind1S,[],[],Rzip0S,Rzip1S,Ytr0,0*Ytr0,Ysh0,Ysh1,[],[],[],[],[]);
SysDataUpd=foldSysData(bus,sw,pv,pq,shunt,line,ind,zip,syn,exc,tg,agc,cac,cluster);
if ~isempty(busTag)&&~isempty(find(busTag==0,1))
% Purge system with busTag
[SysDataUpdFtr,busFtr,swFtr,pvFtr,pqFtr,shuntFtr,lineFtr,indFtr,zipFtr,synFtr,excFtr,tgFtr]=...
filterSysData(busTag,SysData,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(SysData,SysDataUpdFtr,x0,busFtr,swFtr,pvFtr,pqFtr,shuntFtr,lineFtr,indFtr,zipFtr,synFtr,excFtr,tgFtr);
SysData=SysDataUpdFtr;
[SysDataUpd,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);
end
xNew=x0;
if AEmethod==0
[stateNew,finalAlpha,alphaList,diff]=solveAlgebraicHem(SimData,SysData,SysParaSim,x0,xNew);
else
[stateNew,flag,diff,loop]=solveAlgebraicNR(SimData,SysData,SysParaSim,x0,xNew);
if flag==0
finalAlpha=1;
else
finalAlpha=0;
end
alphaList=linspace(0,finalAlpha,loop);
end
[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(stateNew,SysData);
sNew=[s;s0Add];
stateUpd=foldX(SysDataUpd,V,Q,sNew,d,w,eq1,eq2,ed1,ed2,psid,psiq,Pm,Ef,Vavrm,Vavrr,Vavrf,Vavrref,tgovg,tgovm,tgovmech,f,dpg,qplt,vg);
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