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University of Minnesota / Honeywell
Date : October 25th, 2002
Units: lbs.
Units: deg.
Units: deg.
Units: deg.
fi_flag tells nlplant
which Model to use:
0: Low Fidelity
1: High Fidelity
Nonlinear Equations of plant and Aerodynamic Tables :
− Aircraft Control & Simulation, Stevens & Lewis
− NASA Techincal Paper 1538 Nguyen et al., 1973
rad2deg
T
Time
−C−
Thrust Trim Setting
Thrust Saturation
y_sim
States
Scope5
Scope4
Scope3
Scope2
Scope1
Scope
−C−
Rudder Trim Setting
Rudder Saturation
Out1
Rudder Disturbance
statedelta_lef (deg)
Leading Edge Flap
d_LF
LEF deflection
LEF Saturation
1
s
Integrate
F16 State
Derivatives
−C−
Fidelity Flag
MATLAB
Function
F16 nlsim
nlplant
−C−
Elevator Trim Setting
Elevator Saturation
Out1
Elevator Disturbance
emu
emu
surfaces
Control Surface Deflections
0
Clock
−C−
Aileron Trim Setting
Aileron Saturation
Out1
Aileron Disturbance
trim
dist
npos (ft)
epos (ft)
alt (ft)
theta (deg)
psi (deg)
vel (ft/s)
alpha( deg)
beta (deg)
p (deg/s)
q (deg/s)
r (deg/s)
nx (g)
ny (g)
nz (g)
phi (deg)
mach
qbar (lb/ft ft)
ps (lb/ft ft)
%1 )
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6 6 6
6 6 6
6 6 6
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6#
6#
6# : :
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6# 6
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