Biomedical Engineering Reference
In-Depth Information
s T
) = ʥ j L j ʣ 1
y T
) ʣ 1
y
(
r j ,
)
(
r j ,
(
)
(
L j ʥ j
s
t
t
y
t
t
y
= ʥ j L j ʣ 1
L j ʥ j ,
(3.59)
y
y T
where we assume
) = ʣ y .
In this vector case, the unit-gain constraint is expressed as
y
(
t
)
(
t
s T
s
(
r j ,
t
)
(
r j ,
t
) = ʥ j .
(3.60)
Imposing this relationship, we get,
= ʥ j L j ʣ 1
ʥ j
L j ʥ j ,
y
and
L j ʣ 1
L j 1
ʥ j
=
.
(3.61)
y
Substituting the above equation into Eq. ( 3.58 ), we obtain
L j ʣ 1
L j 1 L j ʣ 1
s
(
r j ,
t
) =
y
(
t
).
(3.62)
y
y
Assuming that the model data covariance can be replaced by the sample data covari-
ance R ,Eq.( 3.62 ) is rewritten as
W T
s
(
r
,
t
) =
(
r j )
y
(
t
),
(3.63)
where the weight matrix is given by
L T
1
R 1 L
R 1 L
W
(
r j ) =
(
r j )
(
r j )
(
r j )
.
(3.64)
The weight matrix of the vector array-gain minimum-variance beamformer can be
derived using the array-gain constraint,
s T
s
(
r j ,
t
)
(
r j ,
t
) = ʥ j
L
(
r j ) .
(3.65)
Substituting this relationship into Eq. ( 3.59 ) and using Eq. ( 3.58 ), the resultant weight
matrix is expressed as
L T
1
R 1
L
R 1
L
W
(
r j ) =
(
r j )
(
r j )
(
r j )
.
(3.66)
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