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Navion Lateral State Space Setup - Archangel
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%navion lateral state space setup
%FASAND Fundamentals of Aircraft Simulation And Nonlinear Dynamics
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% This is a state space model of the Navion example aircraft
% used to validate the FASAND code. The A and B matricies were
% obtained from Arcangle 1.0 by inputing the example non-dimensional
% derivatives provided in appendix A of "Flight stability and
% control" Robert C. Nelson
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This Script is free to copy and distribute for educational purposes as long
as this notice is included.
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Doug Hiranaka
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Created: 8-98
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Copyright (c) 1996-98 by Penguin Aeronautics.
ANavionLatA=[ -0.2531035 0.1834322 0
0
-15.86694
0
0
1
0
0
4.519665
0
ANavionLatB=[ 0
0 -1
0
-8.370129 0
0
0
0
2.1844
1
-0.348499 0 -0.75761 ];
0.0704561
0
0
28.73202
2.294273
0
0
-0.2228004 -4.583323 ];
ANavionLatC=[ 1 0 0 0 0
0 1 0 0 0
0 0 1 0 0
0 0 0 1 0
0 0 0 0 1 ];
ANavionLatD=[ 0 0
0 0
0 0
0 0
0 0 ];
states = {’beta’ ’phi’ ’p’ ’psi’ ’r’};
inputs = {’aileron’ ’rudder’};
output = {’sideslip’ ’bank angle’ ’bank rate’ ’yaw angle’ ’yaw rate’};
aLatSys = ss(ANavionLatA,ANavionLatB,ANavionLatC,ANavionLatD,’statename’,states,...
’inputname’,inputs,...
’outpurname’,output);
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