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Control Design for F-18 Longitudinal Dynamics

Compute the open loop system modes and obtain the eigenvalues and eigenvectors

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Added on  2023-05-30

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This document discusses the control design for F-18 Longitudinal Dynamics. It covers topics such as open loop system modes, transfer function, equivalent compensator, root locus and system controllability. The document also provides MATLAB code for computations. The subject is Control Design and the course code is F-18 Longitudinal Dynamics. The document is relevant for students studying this course at any college or university.

Control Design for F-18 Longitudinal Dynamics

Compute the open loop system modes and obtain the eigenvalues and eigenvectors

   Added on 2023-05-30

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Student Name
Student ID Number
CONTROL DESIGN
Institutional Affiliation
F-18 Longitudinal Dynamics
Assignment
Date of submission
Question 1
2018
Control Design for F-18 Longitudinal Dynamics_1
Open loop system modes
A system can be represented using the continuous time domain function or using
the state space. The state space uses matrix notation to represent a system of
signals. The standard state space representation is,
̇x= Ax+ Bu
y=Cx + Du
The open loop system mode does not have a feedback loop. Using MATLAB
software, the F-18 longitudinal dynamics is represented as
d
dt [V
α
q
θ ]=
[0.0239 28.3172 0 32.2
0.0003 0.3621 1 0
0 2.2115 0.2532 0
0 0 1 0 ][V
α
q
θ ]+
[3.8114 0.001
0.0515 0
2.8791 0
0 0 ] [δe
δr ]
[ γ
V ]= [0 1 0 1
1 0 0 0 ] [V
α
q
θ ]
To compute the eigenvalues and eigenvectors,
A=[-0.0239 -28.3172 0 -32.2;-0.0003 -0.3621 1 0;0 -2.2115 -0.2532 0; 0 0 1 0]
B=[-3.8114 0.001; -0.0515 0;-2.8791 0;0 0]
C=[0 -1 0 1;1 0 0 0]
%%Compute the open loop system modes to obtain the eigenvalues and
eigenvectors
[V,D]=eig(A);
disp('EigenValues:')
disp(abs(V))
disp('EigenVector:')
disp(abs(D))
Question 2
1
Control Design for F-18 Longitudinal Dynamics_2
The transfer function of the system is given based on the following relationship,
G ( s ) =K ( n ( s )
sk d ( s ) ) for a system of type K
2x2 system transfer matrix
G11 ( s )=111.4 s3 +1534 s2 1.11e04 s+1.046e04
s448.98 s353.64 s2+3871 s625.1
G12 ( s ) =7.061e05 s3 +1.881e07 s21.868e07 s9.515 e 08
s4 48.98 s353.64 s2+ 3871 s625.1
G2 1 ( s ) = 287.2 s3+ 7640 s2+2038 s741.6
s448.98 s353.64 s2 +3871 s625.1
G22 ( s ) =9.749e05 s3 +2.341e07 s24.209e07 s +2.954 e 07
s448.98 s353.64 s2 +3871 s625.1
Question 3
Single input-single output systems for the transfer function G11(s).
G11 ( s )=111.4 s3 +1534 s2 1.11e04 s+1.046e04
s448.98 s353.64 s2+3871 s625.1
Using the characteristic equation to determine the poles of the system,
poles=[-1.149;-8;-8.5;-9]; %place observer poles
2
Control Design for F-18 Longitudinal Dynamics_3

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