lpv_init_run.m

我自己编写的飞行器控制系统设计代码

%main program of the analysis and synthesis of parmeter dependent 
%lpv controller for Logitudinal dynamic controller of UAV flight
%demonstrator

%generating varying system matrices
LPV_Model_matching;
vparm=viv;
%input/ouput of 2Dof structure

nmeas=3 % number of measure
nctrl=2 % number of control

%calcuate the basis functin 
[fparm,gparm,gradf,gradg]=calcbasis(vparm)
vnu=[-10 10];
[gam,xmat,ymat,xyopt] = lpvsol(vlpv,nmeas,nctrl,vnu,fparm,gparm,gradf,gradg);