F16Manual.pdf
Transcript of F16Manual.pdf
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C
M, q
N, r
L, p
x, u
y, v
z, w
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UniversityofM
innesota/Honeywell
Date:October25th,2002
Units:lbs.
Units:deg.
Units:deg.
Units:deg.
fi_
flagtellsnlplant
whichModeltouse:
0:Low
Fidelity
1:HighFidelity
NonlinearEquationsofplantandAerodynamicTables:
AircraftControl&
Simulation,Stevens&Lewis
NASATechincalPaper1538Nguyenetal.,1973
rad2deg
TTime
C
ThrustTrimSetting
ThrustSaturation
y_sim
States
Scope5
Scope4
Scope3
Scope2
Scope1
Scope
C
RudderTrimSetting
RudderSaturation
Out1
RudderDisturbance
state
delta_
lef(deg)
LeadingEdgeFlap
d_
LF
LEFdeflection
LEFSaturation
1 s
Integrate
F16State
Derivatives
C
FidelityFlag
MATLAB
Function
F16nlsim
nlplant
C
ElevatorTrimSetting
ElevatorSaturation
Out1
ElevatorDisturbance
m
m
surfaces
ControlSurfaceDeflections
0Clock
C
AileronTrimSetting
AileronSaturation
Out1
AileronDisturbance
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/ftft)
ps(lb/ftft)
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0 5 10 15 20 25 302108
2110
2112
2114
2116
2118
2120
2122
delThrust
Time (sec)
Trimed at Velocity = 500.0Alt. = 15000.0
LOFIHIFI
0 5 10 15 20 25 308
6
4
2
0
2
4
delElevator
Time (sec)
Trimed at Velocity = 500.0Alt. = 15000.0
0 5 10 15 20 25 300.1
0.08
0.06
0.04
0.02
0
delAileorn
Time (sec)
Trimed at Velocity = 500.0Alt. = 15000.0
0 5 10 15 20 25 300
0.02
0.04
0.06
0.08
0.1
delRudder
Time (sec)
Trimed at Velocity = 500.0Alt. = 15000.0
0 10 20 300
2000
4000
6000
8000
10000
12000
14000
16000
NorthPos.
Time (sec)
Trimed at Velocity = 500.0Alt. = 15000.0
0 10 20 30500
0
500
1000
1500
2000
2500
3000
EastPos.
Time (sec)
Trimed at Velocity = 500.0Alt. = 15000.0
0 10 20 301.2
1.25
1.3
1.35
1.4
1.45
1.5
1.55x 10
4
Altitudeft
Time (sec)
Trimed at Velocity = 500.0Alt. = 15000.0
LOFIHIFI
0 10 20 300
2
4
6
8
10
12
14
16
PHI(degrees)
Time (sec)
Trimed at Velocity = 500.0Alt. = 15000.0
LOFIHIFI
0 10 20 3040
30
20
10
0
10
THETA(degrees)
Time (sec)
Trimed at Velocity = 500.0Alt. = 15000.0
LOFIHIFI
0 10 20 305
0
5
10
15
20
25
PSI(degrees)
Time (sec)
Trimed at Velocity = 500.0Alt. = 15000.0
LOFIHIFI
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0 10 20 30460
480
500
520
540
560
580
600
Velocity(ft/s)
Time (sec)
Trimed at Velocity = 500.0Alt. = 15000.0
LOFIHIFI
0 10 20 3020
15
10
5
0
5
10
15
20
25
AngleofAttack(degrees)
Time (sec)
Trimed at Velocity = 500.0Alt. = 15000.0
LOFIHIFI
0 10 20 301.5
1
0.5
0
0.5
1
1.5
SideSlip(degrees)
Time (sec)
Trimed at Velocity = 500.0Alt. = 15000.0
LOFIHIFI
0 10 20 3015
10
5
0
5
10
15
Ro
llRate(deg/s)
Time (sec)
Trimed at Velocity = 500.0Alt. = 15000.0
LOFIHIFI
0 10 20 3030
20
10
0
10
20
30
Pitc
hRate(deg/s)
Time (sec)
Trimed at Velocity = 500.0Alt. = 15000.0
LOFIHIFI
0 10 20 304
3
2
1
0
1
2
3
YawRate(deg/s)
Time (sec)
Trimed at Velocity = 500.0Alt. = 15000.0
LOFIHIFI
0 10 20 300.1
0
0.1
0.2
0.3
0.4
0.5
0.6
accx
Time (sec)
Trimed at Velocity = 500.0Alt. = 15000.0
0 10 20 300.1
0.08
0.06
0.04
0.02
0
0.02
0.04
0.06
0.08
accy
Time (sec)
Trimed at Velocity = 500.0Alt. = 15000.0
0 10 20 304
3
2
1
0
1
2
3
4
5
accz
Time (sec)
Trimed at Velocity = 500.0Alt. = 15000.0
0 10 20 300.44
0.46
0.48
0.5
0.52
0.54
0.56
0.58
Mach
Time (sec)
Trimed at Velocity = 500.0Alt. = 15000.0
0 10 20 30160
180
200
220
240
260
280
300
qbar)
Time (sec)
Trimed at Velocity = 500.0Alt. = 15000.0
0 10 20 301180
1200
1220
1240
1260
1280
1300
1320
1340
ps
Time (sec)
Trimed at Velocity = 500.0Alt. = 15000.0
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0 5 10 15 20 25 302108
2110
2112
2114
2116
2118
2120
2122
Thrust
Time (sec)
Trim: Vel. = 500.0Alt. = 15000.0
0 5 10 15 20 25 308
6
4
2
0
2
4
DelElevator
Time (sec)
Trim: Vel. = 500.0Alt. = 15000.0
0 5 10 15 20 25 300.1
0.08
0.06
0.04
0.02
0
DelAileron
Time (sec)
Trim: Vel. = 500.0Alt. = 15000.0
0 5 10 15 20 25 300
0.02
0.04
0.06
0.08
0.1
DelRudder
Time (sec)
Trim: Vel. = 500.0Alt. = 15000.0
LOFIHIFILOFILTIHIFILTI
0 10 20 300
2000
4000
6000
8000
10000
12000
14000
16000
NorthPos.
Time (sec)
Trim: Vel. = 500.0Alt. = 15000.0
0 10 20 30500
0
500
1000
1500
2000
2500
3000
EastPos.
Time (sec)
Trim: Vel. = 500.0Alt. = 15000.0
0 10 20 301.2
1.25
1.3
1.35
1.4
1.45
1.5
1.55x 10
4
Altitudeft
Time (sec)
Trim: Vel. = 500.0Alt. = 15000.0
0 10 20 302
0
2
4
6
8
10
12
14
16
PHI(degrees)
Time (sec)
Trim: Vel. = 500.0Alt. = 15000.0
0 10 20 3040
30
20
10
0
10
20
THETA(degrees)
Time (sec)
Trim: Vel. = 500.0Alt. = 15000.0
0 10 20 305
0
5
10
15
20
25
PSI(degrees)
Time (sec)
Trim: Vel. = 500.0Alt. = 15000.0
LOFIHIFILOFILTIHIFILTI
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0 10 20 30460
480
500
520
540
560
580
600
Velocity(ft/s)
Time (sec)
Trim: Vel. = 500.0Alt. = 15000.0
0 10 20 3020
15
10
5
0
5
10
15
20
25
AngleofAttack(degrees)
Time (sec)
Trim: Vel. = 500.0Alt. = 15000.0
0 10 20 301.5
1
0.5
0
0.5
1
1.5
SideSlip(degrees)
Time (sec)
Trim: Vel. = 500.0Alt. = 15000.0
0 10 20 3015
10
5
0
5
10
15
RollRate(deg/s)
Time (sec)
Trim: Vel. = 500.0Alt. = 15000.0
0 10 20 3030
20
10
0
10
20
30
P
itchRate(deg/s)
Time (sec)
Trim: Vel. = 500.0Alt. = 15000.0
0 10 20 304
3
2
1
0
1
2
3
Y
awRate(deg/s)
Time (sec)
Trim: Vel. = 500.0Alt. = 15000.0
LOFIHIFILOFILTI
HIFILTI
0 10 20 30500
0
500
1000
1500
2000
2500
accx
Time (sec)
Trim: Vel. = 500.0Alt. = 15000.0
0 10 20 302.5
2
1.5
1
0.5
0
0.5
accy
Time (sec)
Trim: Vel. = 500.0Alt. = 15000.0
0 10 20 304
3
2
1
0
1
2
3
4
5
accz
Time (sec)
Trim: Vel. = 500.0Alt. = 15000.0
0 10 20 300.1
0
0.1
0.2
0.3
0.4
0.5
0.6
Mach
Time (sec)
Trim: Vel. = 500.0Alt. = 15000.0
0 10 20 300
50
100
150
200
250
300
qbar)
Time (sec)
Trim: Vel. = 500.0Alt. = 15000.0
0 10 20 30200
0
200
400
600
800
1000
1200
1400
ps
Time (sec)
Trim: Vel. = 500.0Alt. = 15000.0
LOFI
HIFILOFILTIHIFILTI
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25 20 15 10 5 0 53
2
1
0
1
2
3
0.650.880.9450.9720.9860.993
0.998
0.999
0.650.880.9450.9720.9860.993
0.998
0.999
5101520
Altitude = 15000.00 ft Velocity = 500.00 ft/sAll Poles
Blue = lofi Red = hifi.
Real Axis
ImaginaryAxis
25 20 15 10 5 0 51.5
1
0.5
0
0.5
1
1.50.860.9650.9860.9930.996.998
0.999
1
1
0.860.9650.9860.9930.996.998
0.999
1
15101520
Altitude = 15000.00 ft Velocity = 500.00 ft/sLongitudal Directional Poles
Blue = lofi Red = hifi.
Real Axis
ImaginaryAxis
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25 20 15 10 5 03
2
1
0
1
2
30.60.840.920.960.980.99
0.996
0.999
0.60.840.920.960.980.99
0.996
0.999
5101520
Altitude = 15000.00 ft Velocity = 500.00 ft/sLateral Directional Poles
Blue = lofi Red = hifi.
Real Axis
ImaginaryAxis
102
101
100
101
102
1010
105
100
105
LogM
agnitude
Frequency (radians/sec)
102
101
100
101
102
300
250
200
150
100
50
Phase(degrees)
Frequency (radians/sec)
hifilofi
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0 5 10 15 20 25 30 35 40 45 502108
2110
2112
2114
2116
2118
2120
2122
Thrust
Time (sec)
Trim: Vel. = 500.0Alt. = 15000.0
LOFIHIFILOFILTIHIFILTI
0 5 10 15 20 25 30 35 40 45 508
6
4
2
0
2
4
DelElevator
Time (sec)
Trim: Vel. = 500.0Alt. = 15000.0
LOFIHIFILOFILTIHIFILTI
2000
0
2000
4000
6000
8000
0
0.5
1
1.5
2
2.5
3
x 104
1
1.1
1.2
1.3
1.4
1.5
1.6
x 104
East PositionNorth Position
Altitude
LOFIHIFI
0 5 10 15 20 25 30 35 40 45 500.5
0
0.5
1
1.5
2
2.5
3x 10
4
NorthPos.
Time (sec)
Trim: Vel. = 500.0Alt. = 15000.0
LOFIHIFILOFILTIHIFILTI
0 5 10 15 20 25 30 35 40 45 501000
0
1000
2000
3000
4000
5000
6000
7000
8000
EastPos.
Time (sec)
Trim: Vel. = 500.0Alt. = 15000.0
LOFIHIFILOFILTIHIFILTI
0 5 10 15 20 25 30 35 40 45 501.2
1.25
1.3
1.35
1.4
1.45
1.5
1.55x 10
4
Altitudeft
Time (sec)
Trim: Vel. = 500.0Alt. = 15000.0
LOFIHIFILOFILTIHIFILTI
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0 5 10 15 20 25 30 35 40 45 50440
460
480
500
520
540
560
580
600
Velocity(ft/s)
Time (sec)
Trim: Vel. = 500.0Alt. = 15000.0
LOFIHIFILOFILTIHIFILTI
0 5 10 15 20 25 30 35 40 45 5020
15
10
5
0
5
10
15
20
25
AngleofAttack(degrees)
Time (sec)
Trim: Vel. = 500.0Alt. = 15000.0
LOFIHIFILOFILTIHIFILTI
0 5 10 15 20 25 30 35 40 45 501.5
1
0.5
0
0.5
1
1.5
SideSlip(degrees)
Time (sec)
Trim: Vel. = 500.0Alt. = 15000.0
LOFIHIFILOFILTIHIFILTI
0 5 10 15 20 25 30 35 40 45 502
0
2
4
6
8
10
12
14
16
PHI(degrees)
Time (sec)
Trim: Vel. = 500.0Alt. = 15000.0
LOFIHIFILOFILTIHIFILTI
0 5 10 15 20 25 30 35 40 45 5040
30
20
10
0
10
20
THETA(degrees)
Time (sec)
Trim: Vel. = 500.0Alt. = 15000.0
LOFIHIFILOFILTIHIFILTI
0 5 10 15 20 25 30 35 40 45 505
0
5
10
15
20
25
30
35
PSI(degrees)
Time (sec)
Trim: Vel. = 500.0Alt. = 15000.0
LOFIHIFILOFILTIHIFILTI
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0 5 10 15 20 25 30 35 40 45 5015
10
5
0
5
10
15
RollRate(deg/s)
Time (sec)
Trim: Vel. = 500.0Alt. = 15000.0
LOFIHIFILOFILTIHIFILTI
0 5 10 15 20 25 30 35 40 45 5030
20
10
0
10
20
30
PitchRate(deg/s)
Time (sec)
Trim: Vel. = 500.0Alt. = 15000.0
LOFIHIFILOFILTIHIFILTI
0 5 10 15 20 25 30 35 40 45 504
3
2
1
0
1
2
3
YawRate(deg/s)
Time (sec)
Trim: Vel. = 500.0Alt. = 15000.0
LOFIHIFILOFILTIHIFILTI
0 5 10 15 20 25 30 35 40 45 50500
0
500
1000
1500
2000
2500
accx
Time (sec)
Trim: Vel. = 500.0Alt. = 15000.0
LOFIHIFILOFILTIHIFILTI
0 5 10 15 20 25 30 35 40 45 502.5
2
1.5
1
0.5
0
0.5
accy
Time (sec)
Trim: Vel. = 500.0Alt. = 15000.0
LOFIHIFILOFILTIHIFILTI
0 5 10 15 20 25 30 35 40 45 504
3
2
1
0
1
2
3
4
5
accz
Time (sec)
Trim: Vel. = 500.0Alt. = 15000.0
LOFIHIFILOFILTIHIFILTI
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0 5 10 15 20 25 30 35 40 45 50200
0
200
400
600
800
1000
1200
1400
ps
Time (sec)
Trim: Vel. = 500.0Alt. = 15000.0
LOFIHIFILOFILTIHIFILTI
0 5 10 15 20 25 30 35 40 45 5050
0
50
100
150
200
250
300
qbar)
Time (sec)
Trim: Vel. = 500.0Alt. = 15000.0
LOFIHIFILOFILTIHIFILTI
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