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Characteristic values

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Char. eq of a system is det(sI-A)=0 the polynomial det(sI-A) is called char. pol. the roots of char. eq. are char. values they are also the eigen-values of A – PowerPoint PPT presentation

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Title: Characteristic values


1
Characteristic values
  • Char. eq of a system is
  • det(sI-A)0
  • the polynomial det(sI-A) is called char. pol.
  • the roots of char. eq. are char. values
  • they are also the eigen-values of A
  • e.g.
  • ? (s1)(s2)2 is the char. pol.
  • (s1)(s2)20 is the char. eq.
  • s1-1,s2-2,s3-2 are char. values or eigenvalues

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gtgt MySysss(A,B,C,D) a x1 x2 x3 x1
-1 0 0 x2 0 -2 1 x3 0 0 -2 b
u1 x1 1 x2 0 x3 1 c
x1 x2 x3 y1 1 1 1 d u1
y1 0 Continuous-time model.
gtgt A-1 0 0 0 -2 1 0 0 -2 A -1 0
0 0 -2 1 0 0 -2 gtgt
B101 B 1 0 1 gtgt C1 1
1 C 1 1 1 gtgt D0 D 0
4
gtgt tf(MySys) Transfer function 2 s2 8 s
7 --------------------- s3 5 s2 8 s 4 gtgt
zpk(MySys) Zero/pole/gain 2 (s2.707)
(s1.293) --------------------- (s1)
(s2)2 gtgt roots(2 8 7) ans -2.7071
-1.2929 gtgt roots(1 5 8 4) ans -2.0000
-2.0000 -1.0000
gtgt ssym('s') s s gtgt det(seye(3)-A) ans
(s1)(s2)2 gtgt eig(A) ans -1 -2
-2 gtgt DCinv(seye(3)-A)B ans
1/(s1)1/(s2)21/(s2) gtgt simplify(ans) ans
(2s28s7)/(s1)/(s2)2
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gtgt inv(seye(3)-A) ans 1/(s1), 0,
0 0,
1/(s2), 1/(s2)2 0,
0, 1/(s2) gtgt ilaplace(ans) ans
exp(-t), 0, 0
0, exp(-2t),
texp(-2t) 0, 0,
exp(-2t) gtgt tsym('t') t t gtgt
expm(At) ans exp(-t), 0,
0 0,
exp(-2t), texp(-2t) 0,
0, exp(-2t)
6
gtgt expm(At)A ans -exp(-t),
0, 0
0,
-2exp(-2t), exp(-2t)-2texp(-2t)
0, 0,
-2exp(-2t) gtgt
Aexpm(At) ans -exp(-t),
0, 0
0,
-2exp(-2t), exp(-2t)-2texp(-2t)
0, 0,
-2exp(-2t) gtgt
Aexpm(At)-expm(At)A ans 0, 0, 0 0,
0, 0 0, 0, 0
7
can
?
set t0
?No
can
?
v
at t0
?
v
8
Solution of state space model
  • Recall sX(s)-x(0)AX(s)BU(s)
  • (sI-A)X(s)BU(s)x(0)
  • X(s)(sI-A)-1BU(s)(sI-A)-1x(0)
  • x(t)(L-1(sI-A)-1))Bu(t) L-1(sI-A)-1) x(0)
  • x(t) eA(t-t)Bu(t)d teAtx(0)
  • y(t) CeA(t-t)Bu(t)d tCeAtx(0)Du(t)

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S.S to T.F.
  • X(s)(sI-A)-1BU(s)
  • Y(s)C(sI-A)-1BU(s)DU(s)
  • (D C(sI-A)-1B)U(s)
  • ? T.F. H(s) D C(sI-A)-1B
  • In matlab ss2tf
  • eig
  • roots
  • poly
  • use help to find out how to use these

10
  • In Matlab
  • gtgt A0 1-2 -3
  • gtgt B01
  • gtgt C1 3
  • gtgt D0
  • gtgt n,dss2tf(A,B,C,D)
  • n
  • 0 3.0000 1.0000
  • d
  • 1 3 2
  • gtgttf(n,d)

11
But dont use those for hand calculation
  • useX(s)(sI-A)-1BU(s)(sI-A)-1x(0)
  • x(t)L-1(sI-A)-1BU(s)L-1 (sI-A)-1
    x(0)
  • Y(s)C(sI-A)-1BU(s)DU(s)C(sI-A)-1x(0)
  • y(t) L-1C(sI-A)-1BU(s)DU(s)CL-1
    (sI-A)-1 x(0)
  • e.g.

u unit step
12
Note T.F.D C(sI-A)-1B
13
Eigenvalues, eigenvectors
  • Given a nxn square matrix A, p is an eigenvector
    of A if Ap?p
  • i.e. ? s.t. Ap ?p
  • ?is an eigenvalue of A
  • Example ,
  • Let ,
  • ?p1 is an e-vector, the e-value1
  • Let ,
  • ?p2 is also an e-vector, assoc. with the ? -2

14
  • In general, if ?, p is an e-pair for A,
  • Ap ?p
  • ?p-Ap0
  • ?Ip-Ap0
  • (?I-A)p0
  • ? p?0 ? det(?I-A)0
  • ? ? is a sol. of char. eq of A
  • char. pol. of nxn A has degn
  • ? A has n eigen-values.
  • e.g. A , det(?I-A)(?-1)(?2)0
  • ? ?11, ?2-2

15
  • If ?1 ??2 ??3?
  • then the corresponding p1, p2, ? will be
    linearly independent, i.e., the matrix
  • Pp1?p2 ? ?pn will be invertible.
  • Ap1 ?1p1
  • Ap2 ?2p2
  • ?
  • Ap1?p2 ? ?Ap1?Ap2 ? ?
  • ?p1? ?p2 ? ?
  • p1 p2 ?

16
  • ? APP?
  • P-1AP ?diag(?1, ?2, ?)
  • ?If A has n lin. ind. Eigenvectors then A can be
    diagonalized.
  • Note Not all square matrices can be diagonalized.

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Example
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  • In Matlab
  • gtgt A2 0 1
  • 0 2 1
  • 1 1 4
  • gtgt P,Deig(A)
  • P
  • 0.6280 0.7071 0.3251
  • 0.6280 -0.7071 0.3251
  • -0.4597 -0.0000 0.8881
  • p1 p2 p3
  • D
  • 1.2679 0 0
  • 0 2.0000 0
  • 0 0 4.7321

?1
?2
?3
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  • If A does not have n lin. ind. e-vectors
  • (some of the eigenvalues are identical),
  • then A can not be diagonalized
  • E.g. A
  • det(?I-A) ?456?31152?210240?32768
  • ?1-8
  • ?2-16
  • ?3-16
  • ?4-16
  • by solving (?I-A)P0

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  • If we use P,Deig(A)
  • get approximate but wrong answer
  • Should use gtgtP,Jjordan(A)
  • P
  • 0.3750 0 1 0.625
  • 0 8 4 0
  • -0.375 0 0 0.375
  • 0 16 9 0
  • J
  • -8 0 0 0
  • 0 -16 1 0
  • 0 0 -16 1
  • 0 0 0 -16

a 3x3 Jordan block assoc. w/. ?-16
31
More Matlab Examples
  • gtgt ssym('s')
  • gtgt A0 1-2 -3
  • gtgt det(seye(2)-A)
  • ans
  • s23s2
  • gtgt factor(ans)
  • ans
  • (s2)(s1)

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  • gtgt P,Deig(A)
  • P
  • 0.7071 -0.4472
  • -0.7071 0.8944
  • D
  • -1 0
  • 0 -2
  • gtgt P,Djordan(A)
  • P
  • 2 -1
  • -2 2
  • D
  • -1 0
  • 0 -2

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  • A 0 1
  • -2 -3
  • gtgt exp(A)
  • ans
  • 1.0000 2.7183
  • 0.1353 0.0498
  • gtgt expm(A)
  • ans
  • 0.6004 0.2325
  • -0.4651 -0.0972
  • gtgt tsym('t')
  • gtgt expm(At)
  • ans
  • -exp(-2t)2exp(-t),
    exp(-t)-exp(-2t)
  • -2exp(-t)2exp(-2t), 2exp(-2t)-exp(-t)

?
34
v
v
35
Similarity transformation
same system as()
36
Example
diagonalized
decoupled
37
Invariance
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Controllability
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Example
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  • In Matlab
  • gtgt Sctrb(A,B)
  • gtgt rrank(S)
  • If S is square (when B is nx1)
  • gtgt det(S)

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Observability
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Example
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  • In Matlab
  • gtgt Vobsv(C,A)
  • gtgt rrank(V)
  • rank must n
  • Or if single output (ie V is square), can use
  • gtgt det(V)
  • det must be nonzero

Lookfor controllability Lookfor observability
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  • Recall linear transformation
  • Controllabilitybeing able to use u(t) to drive
    any state to origin in finite time
  • Observabilitybeing able to computer any x(0)
    from observed y(t)
  • After transformation, eigenvalues, char. poly,
    char. eq, char. values, T.F., poles, zeros
    un-changed, but eigenvector changed

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  • Controllability is invariant under transf.

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  • Observability invariant under transf.

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State Feedback
D
1 s
r
u
x



y
B
C


-
A
K
feedback from state x to control u
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  • In Matlab
  • Given A,B,C,D
  • ?Compute QCctrb(A,B)
  • ?Check rank(QC)
  • If it is n, then
  • ?Select any n eigenvalues(must be in complex
    conjugate pairs)
  • ev?1 ?2 ?3 ?n
  • ?Compute
  • Kplace(A,B,ev)

ABk will have eigenvalues at
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  • Thm Controllability is unchanged after state
    feedback.
  • But observability may change!
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