clear all
close all
load modelLong aL bL cL dL Vt Hp aircraft % Load lateral directional subsystem linear model
Lsys=ss(aL,bL,cL,dL);
set(Lsys,'statename',{'u(f/s)' 'w(f/s)' 'q(r/s)' 'thet(r)' 'h(f)'})
set(Lsys,'inputname',{'deltaE(r)' 'Bhp(hp)'})
set(Lsys,'outputname',{'u(f/s)' 'w(f/s)' 'q(r/s)' 'thet(r)' 'h(f)' 'Vt(f/s)' 'alf(r)' 'gam(r)'})
Lsys
[Wn,Z,Poles]=damp(Lsys)
Ltfsys=tf(Lsys)
Lzpksys=zpk(Lsys)
