The International Archives of the Photogrammetry, Remote Sensing and Spatial Information Sciences. Vol. XXXVII. Part B7. Beijing 2008
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process of function optimization, which is a really tough task in
data processing of the conventional DInSAR.
3.2 Parameter Adjustment by LS Solution
With equation (3) we can compute the increments of elevation
errors and linear deformation velocities along all the arcs in the
network. By trials with simulated data, we have found that the
arcs have an accurate solution for As and Av if y is larger
than 0.45. The network can then be treated in a similar way as a
leveling or GPS network; a weighted LS adjustment is applied
to eliminate geometric inconsistency due to uncertainty in phase
data, and thus obtaining the most probable values of the linear
deformation velocities and elevation errors at PSs.
Taking the adjustment of LOS linear deformation velocities as
an example, we present here some basic ideas for computation.
A prototype observation equation for an arc is expressed as
Vp-v, =Av pl +r pl , p*l,Vp,l = \,2,K ,K (4)
where v p = linear deformation velocity at PS p
v, = linear deformation velocity at PS /
K= total number of all the PSs
Suppose there are Q arcs available in the network, we will have
Q observation equations. The MC value of each arc can be used
as a weight. With a weighted LS solution, the motion velocities
at all the K PS can be eventually obtained. Such procedure can
also be applied in a similar way onto the elevation-
inconsistency network to estimate the elevation errors at all the
K PSs. The Kriging interpolator can be applied to generate the
deformation-velocity map and the elevation-error map.
As a remark, we underline that a reference point without motion
or elevation error should be selected according to a priori
information to obtain a unique solution with LS adjustment, and
thus making all the estimates be related to the benchmark. In
addition, we solved the large sparse matrix system using the
software package termed UMFPACK (Davis, 2002). Moreover,
it should be noted that the FCN used here is much stronger in
terms of reliability than the TIN. Our simulation study shows
that the LS solution derived with the FCN is much more
accurate than that derived with the TIN even though a small
portion of measurements ( Ae , Av ) are intentionally set as
outliers. This is because the redundancy number in the FCN is
significantly larger than that in the TIN.
3.3 Separation of Nonlinear Deformation and Atmospheric
Effect
The further analysis focuses on isolating nonlinear motion from
atmospheric delay. For each interferometric pair, the residual
phase increment (gradient) at each arc can be first derived. The
integration of gradients (i.e., phase unwrapping) of all the arcs
in the network is then performed by a weighted least squares
method (Ghiglia & Pritt, 1998), and thus obtaining the residual
phases in absolute sense at all the PS pixels for each pair. As
mentioned before, the residual phase is contributed by nonlinear
deformation, atmospheric delay and decorrelation noise.
It is possible to separate nonlinear motion from atmospheric
delay because the two terms have different spectral structure in
space and time domain (Ferretti et al., 2000; Mora et al., 2003).
In terms of atmospheric perturbation, a high correlation exhibits
in space, but a significantly low correlation presents in time. In
terms of nonlinear deformation, a strong correlation exists in
space and a high correlation occurs in time. It is however not
easy to discriminate the spectral bands between the nonlinear
deformation and the atmospheric effect without availability of a
priori information. Although an exact separation of the two
terms is a challenged task, we try to achieve such purpose by
introducing a strategy referred to as empirical mode
decomposition (EMD) which was pioneered by Huang et al.
(1998). This method is in principle different from the cascade
filter applied by the previous studies (Ferretti et al., 2000, 2001;
Mora et al., 2003).
To decouple signatures at each PS, we first estimate the time
series of unwrapped residual phases corresponding to all the
SAR acquisition times. This can be done using a singular value
decomposition (SVD) method (for details, see Berardino et al.,
2002). The separation between atmospheric delay and nonlinear
motion is then conducted by EMD using the time series of
unwrapped residual phases.
The dataset being dealt with generally has several features: (a)
the tens of samples are irregular; (b) the data is non-stationary
(varying undulation); and (c) the data represents a nonlinear
process. Theoretical study by Huang et al. (1998) indicated that
the EMD approach is more advantageous for dealing with a
nonlinear and nonstationary process than other signal analysis
tools like Fourier transform. The EMD method separates the
signal into a collection of intrinsic mode functions (IMF) that
are useful for revealing some physical properties. For details of
EMD operation, see Huang et al., 1998.
By trials with real data, we can generally extract four IMFs
from the time series of unwrapped residual phases. The IMFs
with high frequencies correspond to atmospheric component,
while the IMFs with low frequencies reflect nonlinear motion.
It is not so direct to thoroughly discriminate them in the case of
no a priori information available. However, reasonable results
have been produced in our case when we consider the sum of
the first and second level of IMFs as the atmospheric phases
and treat the sum of the third and fourth level of IMFs as the
nonlinear motions. The obtained two time series of phases for
nonlinear motion and atmospheric delay at each PS are
expressed as
r ,def {t) = W n,def {t 0 ),r ,def {t x ),A (5)
y,°‘ m {t) = \r ,m {t»\r ,m {t,),A ,r ,m {t N )} (6)
where y/ nldef (t i ) = phase for nonlinear motion at (imaging time)
y/ a,m (t i ) = phase for atmospheric delay at t,■ (imaging time)
Finally, the total LOS deformation at any PS can be computed
by summing the linear and nonlinear components, which can be
written as a function of SAR acquisition time t t by
def{t i ) = {t i -t Q )-v + ^-^ Mef ( ti ) (7)