NonlinearBook10pt November 20, 2007
ADVANCED STABILITY THEORY 217
us to unify autonomous partial stability theory with time-varying stability
theory. Lyapunov (respectively, asymptotic) stability with respect to x
1
given in Definition 4.1 is referred to in [448] as x
1
-stability (respectively, x
1
-
asymptotic stability) for large x
2
while Lyapunov (respectively, asymptotic)
stability with respect to x
1
uniformly in x
20
given in Definition 4.1 is referred
to in [448] as x
1
-stability (respectively, x
1
-asymptotic stability) with respect
to the whole of x
2
. Note that if a nonlinear dynamical system is Lyapunov
(respectively, asymptotically) stable with respect to x
1
in the sense of
Definition 4.1, then the system is x
1
-stable (respectively, x
1
-asymptotically
stable) in the sense of the definition given in [374, 448]. Furthermore, if
there exist a continuously differentiable function V : D × R
n
2
→ R and a
class K function α(·) (respectively, class K functions β(·) and γ(·)) such
that V (0, 0) = 0 and (4.9) and (4.10) (respectively, (4.9), (4.11), and
(4.15)) hold, then the nonlinear dynamical system (4.6) and (4.7) is x
1
-
stable (respectively, uniformly asymptotically x
1
-stable with respect to x
20
)
in the sense of the definition given in [448]. It is important to note that
the condition V (0, x
2
) = 0, x
2
∈ R
n
2
, allows us to prove partial stability
in the sense of Definition 4.1. Finally, an additional difference between our
formulation of the partial stability problem and the partial stability problem
considered in [374, 448] is in the treatment of the equilibrium of (4.6) and
(4.7). Specifically, in our formulation, we require the partial equilibrium
condition f
1
(0, x
2
) = 0 for every x
2
∈ R
n
2
, whereas in [374,448], th e authors
require the equilibrium cond ition f
1
(0, 0) = 0 and f
2
(0, 0) = 0.
Example 4.1. In this example, we use Theorem 4.1 to show that
the rotational/translational proof-mass model (4.4) and (4.5) is partially
Lyapunov stable with respect to q, ˙q, and
˙
θ. To show this, let x
1
= q,
x
2
= ˙q, x
3
= θ, x
4
=
˙
θ and consider the Lyapunov function candidate
V (x
1
, x
2
, x
3
, x
4
) =
1
2
[kx
2
1
+ (M + m)x
2
2
+ (I + me
2
)x
2
4
+ 2mex
2
x
4
cos x
3
].
(4.20)
Note that V (x
1
, x
2
, x
3
, x
4
) =
1
2
kx
2
1
+
1
2
˜x
T
P (x
3
)˜x, where ˜x = [x
2
x
4
]
T
and
P (x
3
) =
M + m me cos x
3
me cos x
3
I + me
2
. (4.21)
Since
2λ
min
(P (x
3
)) = M + m + I + me
2
−
p
(M + m − I − me
2
)
2
+ 4m
2
e
2
cos
2
x
3
, (4.22)
2λ
max
(P (x
3
)) = M + m + I + me
2
+
p
(M + m − I − me
2
)
2
+ 4m
2
e
2
cos
2
x
3
, (4.23)
it follows that α
min
I
2
≤ 2P (x
3
) ≤ α
max
I
2
, x
3
∈ R, where
α
min
△
= M + m + I + me
2
−
p
(M + m − I − me
2
)
2
+ 4m
2
e
2
, (4.24)