Global Positioning System Reference
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and then setting this quantity equal to zero to obtain:
(
)
1
$
T
T
xHHHy
=
(A.5)
where it is assumed that the matrix inverse involved exists (i.e., that H T H is not sin-
gular).
The estimate described by (A.5) is referred to as a least squares estimate , since,
as shown in (A.3), it results in the minimum square error between the measurement
vector y and Hx , where the latter is the expected measurement vector based upon the
estimate of x .
Next, consider the more general case where the measurement errors are still
Gaussian distributed with zero-mean but are not necessarily identically distributed
or independent of each other. In this case, the maximum likelihood estimate can be
expressed as
1
2
1
(
)
T
1
(
)
yHx R yHx
$
n
x
=
arg max
e
()
12
N
2
x
(A.6)
2
π
R
n
(
)
T
(
)
1
=
arg min
yHxR
n yHx
x
where R n is the covariance matrix associated with the measurement errors and | R n |is
its determinant.
Proceeding as before, (A.6) can be solved to yield:
(
)
1
$
xHRHHRy
n
=
T
1
T
1
(A.7)
n
The estimate in (A.7) is referred to as a WLS solution.
Reference
[1]
Stark, H., and J. W. Woods, Probability, Random Processes, and Estimation Theory for
Engineers , Englewood Cliffs, NJ: Prentice-Hall, 1986.
 
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