Simulink Summary Report

The MathWorks

Table of Contents

1.1. Systems
1.2. Blocks
1.3. Data and Functions
1.4. Signals
1.5. Scopes

List of Tables
1-1. Block Type Count
1-2. Model Functions
1-3. Model Variables

List of Figures
1-1. Angle of Attack
1-2. Pilot G force Scope
1-3. Stick Input

Chapter 1. Model - f14

Solver ode45	ZeroCross on	StartTime 0.0 StopTime 60
RelTol 1e-4	AbsTol 1e-6	Refine 1
InitialStep auto	FixedStep auto	MaxStep auto

NumModelInputs	1	NumModelOutputs	2
NumVirtualSubsystems	5	NumNonvirtSubsystems	0
NumNonVirtBlocksInModel	42	NumBlockTypeCounts	10
NumBlockSignals	22	NumBlockParams	41
NumZCEvents	0	NumNonsampledZCs	0

1.1. Systems

Name	Blocks	Description
Aircraft Dynamics Model	Elevator Deflection d (deg) Vertical Gust wGust (ft/sec) Rotary Gust qGust (rad/sec) Gain3 Gain4 Gain5 Gain6 Sum1 Sum2 Transfer Fcn.1 Transfer Fcn.2 Vertical Velocity w (ft/sec) Pitch Rate q (rad/sec)
Controller	Stick Input (in) alpha (rad) q (rad/sec) Alpha-sensor Low-pass Filter Gain Gain2 Gain3 Pitch Rate Lead Filter Proportional plus integral compensator Stick Prefilter Sum Sum1 Sum2 Elevator Command (deg)
Dryden Wind Gust Models	Band-Limited White Noise Q-gust model W-gust model Wg Qg
f14	u Actuator Model Aircraft Dynamics Model Angle of Attack Controller Dryden Wind Gust Models Gain Gain1 Gain2 Gain5 More Info More Info1 Nz pilot calculation Pilot Pilot G force Scope Stick Input Sum Sum1 alpha (rad) Nz Pilot (g)
More Info
More Info1
Nz pilot calculation	w q Constant Derivative Derivative1 Gain1 Gain2 Product Sum1 Pilot g force (g)

1.2. Blocks

Name	BlockType	Parent	OutputSignalNames
Gain	Gain	f14/Controller	<1115.00171>
Gain2	Gain	f14/Controller	<1117.00146>
Gain3	Gain	f14/Controller	<1119.00146>
Sum	Sum	f14/Controller	<1122.00183>
Sum1	Sum	f14/Controller	<1125.00183>
Sum2	Sum	f14/Controller	<1128.00146>
Gain	Gain	f14	<1105.00146>
Gain1	Gain	f14	<1096.00146>
Gain2	Gain	f14	<1107.00146>
Gain5	Gain	f14	<1112.00159>
Nz Pilot (g)	Outport	f14
Pilot	SignalGenerator	f14	<1103.00146>
Stick Input	Scope	f14
Sum	Sum	f14	<1099.00146>
Sum1	Sum	f14	<1083.00256>
alpha (rad)	Outport	f14
Actuator Model	TransferFcn	f14	<1089.00183>
Elevator Deflection d (deg)	Inport	f14/Aircraft Dynamics Model	<1132.00146>
Gain3	Gain	f14/Aircraft Dynamics Model	<1134.00146>
Gain4	Gain	f14/Aircraft Dynamics Model	<1136.00134>
Gain5	Gain	f14/Aircraft Dynamics Model	<1138.00134>
Gain6	Gain	f14/Aircraft Dynamics Model	<1140.00134>
Pitch Rate q (rad/sec)	Outport	f14/Aircraft Dynamics Model
Rotary Gust qGust (rad/sec)	Inport	f14/Aircraft Dynamics Model	<1142.00134>
Sum1	Sum	f14/Aircraft Dynamics Model	<1146.00134>
Sum2	Sum	f14/Aircraft Dynamics Model	<1150.00134>
Transfer Fcn.1	TransferFcn	f14/Aircraft Dynamics Model	<1152.00134>
Transfer Fcn.2	TransferFcn	f14/Aircraft Dynamics Model	<1154.00134>
Vertical Gust wGust (ft/sec)	Inport	f14/Aircraft Dynamics Model	<1155.00134>
Vertical Velocity w (ft/sec)	Outport	f14/Aircraft Dynamics Model
Angle of Attack	Scope	f14
Alpha-sensor Low-pass Filter	TransferFcn	f14/Controller	<1159.00122>
Elevator Command (deg)	Outport	f14/Controller
Pitch Rate Lead Filter	TransferFcn	f14/Controller	<1162.00134>
Proportional plus integral compensator	TransferFcn	f14/Controller	<1164.00488>
Stick Input (in)	Inport	f14/Controller	<1165.00781>
Stick Prefilter	TransferFcn	f14/Controller	<1167.00159>
alpha (rad)	Inport	f14/Controller	<1168.00159>
q (rad/sec)	Inport	f14/Controller	<1169.00159>
Band-Limited White Noise	SubSystem	f14/Dryden Wind Gust Models	<1170.00159>
Q-gust model	TransferFcn	f14/Dryden Wind Gust Models	<1172.00159>
Qg	Outport	f14/Dryden Wind Gust Models
W-gust model	TransferFcn	f14/Dryden Wind Gust Models	<1175.00159>
Wg	Outport	f14/Dryden Wind Gust Models
Constant	Constant	f14/Nz pilot calculation	<1177.00134>
Derivative	Derivative	f14/Nz pilot calculation	<1179.00134>
Derivative1	Derivative	f14/Nz pilot calculation	<1181.00366>
Gain1	Gain	f14/Nz pilot calculation	<1183.00195>
Gain2	Gain	f14/Nz pilot calculation	<1185.00171>
Pilot g force (g)	Outport	f14/Nz pilot calculation
Product	Product	f14/Nz pilot calculation	<1189.00159>
Sum1	Sum	f14/Nz pilot calculation	<1193.00159>
q	Inport	f14/Nz pilot calculation	<1194.00159>
w	Inport	f14/Nz pilot calculation	<1195.00159>
Pilot G force Scope	Scope	f14
u	Inport	f14	<1102.00146>

Table 1-1. Block Type Count

BlockType	# of Occurrences
Gain	13
TransferFcn	9
Inport	9
Sum	8
Outport	8
SubSystem	7
Scope	3
Derivative	2
SignalGenerator	1
Product	1
Constant	1

1.3. Data and Functions

Table 1-2. Model Functions

Function Name	Parent Blocks	Calling string
pi	Q-gust model Q-gust model	pi/(4b)[1 0] [1 piVto/(4b)]
sqrt	W-gust model	Swg/sqrt(a^3)[sqrt(3)a,1]

Function Name

Parent Blocks

Calling string

Q-gust model
Q-gust model

pi/(4*b)*[1 0]
[1 pi*Vto/(4*b)]

sqrt

W-gust model

Swg/sqrt(a^3)*[sqrt(3)*a,1]

Table 1-3. Model Variables

Variable Name	Parent Blocks	Calling string	Value
Ka	Gain3	Ka	0.677
Kf	Gain	Kf	-1.746
Ki	Proportional plus integral compensator	[Ki]	-3.864
Kq	Gain2	Kq	0.8156
Md	Gain6	Md	-6.8847
Mq	Transfer Fcn.1 Gain1	[1,-Mq] Mq	-0.6571
Mw	Gain4 Gain2	Mw Mw	-0.00592
Swg	W-gust model	Swg/sqrt(a^3)[sqrt(3)a,1]	3
Ta	Actuator Model	[ Ta, 1]	0.05
Tal	Alpha-sensor Low-pass Filter	[Tal,1]	0.3959
Ts	Stick Prefilter	[Ts,1]	0.1
Uo	Gain3 Gain5 Constant	Uo 1/Uo Uo	689.4
Vto	Q-gust model	[1 piVto/(4b)]	690.4
W1	Pitch Rate Lead Filter	[1,W1]	2.971
W2	Pitch Rate Lead Filter	[1,W2]	4.144
Zd	Gain5	Zd	-63.9979
Zw	Transfer Fcn.2 Gain	[1,-Zw] Zw	-0.6385
a	W-gust model W-gust model	Swg/sqrt(a^3)[sqrt(3)a,1] [1 (2/a) 1/a^2]	2.5348
b	Q-gust model Q-gust model	pi/(4b)[1 0] [1 piVto/(4b)]	64.13
g	Gain2	1/g	32.2

1.4. Signals

Name	ParentBlock	RTWStorageClass
<1083.0026>	f14/Sum1	Auto
<1087.002>	f14/Controller	Auto
<1089.0018>	f14/Actuator Model	Auto
<1096.0015>	f14/Gain1	Auto
<1099.0015>	f14/Sum	Auto
<1102.0015>	f14/u	Auto
<1103.0015>	f14/Pilot	Auto
<1105.0015>	f14/Gain	Auto
<1107.0015>	f14/Gain2	Auto
<1110.0016>	f14/Nz pilot calculation	Auto
<1112.0016>	f14/Gain5	Auto
<1115.0017>	f14/Controller/Gain	Auto
<1117.0015>	f14/Controller/Gain2	Auto
<1119.0015>	f14/Controller/Gain3	Auto
<1122.0018>	f14/Controller/Sum	Auto
<1125.0018>	f14/Controller/Sum1	Auto
<1128.0015>	f14/Controller/Sum2	Auto
<1132.0015>	f14/Aircraft Dynamics Model/Elevator Deflection d (deg)	Auto
<1134.0015>	f14/Aircraft Dynamics Model/Gain3	Auto
<1136.0013>	f14/Aircraft Dynamics Model/Gain4	Auto
<1138.0013>	f14/Aircraft Dynamics Model/Gain5	Auto
<1140.0013>	f14/Aircraft Dynamics Model/Gain6	Auto
<1142.0013>	f14/Aircraft Dynamics Model/Rotary Gust qGust (rad//sec)	Auto
<1146.0013>	f14/Aircraft Dynamics Model/Sum1	Auto
<1150.0013>	f14/Aircraft Dynamics Model/Sum2	Auto
<1152.0013>	f14/Aircraft Dynamics Model/Transfer Fcn.1	Auto
<1154.0013>	f14/Aircraft Dynamics Model/Transfer Fcn.2	Auto
<1155.0013>	f14/Aircraft Dynamics Model/Vertical Gust wGust (ft//sec)	Auto
<1159.0012>	f14/Controller/Alpha-sensor Low-pass Filter	Auto
<1162.0013>	f14/Controller/Pitch Rate Lead Filter	Auto
<1164.0049>	f14/Controller/Proportional plus integral compensator	Auto
<1165.0078>	f14/Controller/Stick Input (in)	Auto
<1167.0016>	f14/Controller/Stick Prefilter	Auto
<1168.0016>	f14/Controller/alpha (rad)	Auto
<1169.0016>	f14/Controller/q (rad//sec)	Auto
<1170.0016>	f14/Dryden Wind Gust Models/Band-Limited White Noise	Auto
<1172.0016>	f14/Dryden Wind Gust Models/Q-gust model	Auto
<1175.0016>	f14/Dryden Wind Gust Models/W-gust model	Auto
<1177.0013>	f14/Nz pilot calculation/Constant	Auto
<1179.0013>	f14/Nz pilot calculation/Derivative	Auto
<1181.0037>	f14/Nz pilot calculation/Derivative1	Auto
<1183.002>	f14/Nz pilot calculation/Gain1	Auto
<1185.0017>	f14/Nz pilot calculation/Gain2	Auto
<1189.0016>	f14/Nz pilot calculation/Product	Auto
<1193.0016>	f14/Nz pilot calculation/Sum1	Auto
<1194.0016>	f14/Nz pilot calculation/q	Auto
<1195.0016>	f14/Nz pilot calculation/w	Auto
q	f14/Aircraft Dynamics Model	Auto
qGust	f14/Dryden Wind Gust Models	Auto
w	f14/Aircraft Dynamics Model	Auto
wGust	f14/Dryden Wind Gust Models	Auto

1.5. Scopes

Figure 1-1. Angle of Attack

Figure 1-2. Pilot G force Scope

Figure 1-3. Stick Input