.
The International Archives of the Photogrammetry, Remote Sensing and Spatial Information Sciences. Vol. XXXVII. Part Bl. Beijing 2008
should less than 1. Experiments show the result is optimum
when a value gets 0.1 or so.
2.2.2 registration with least square fitting method
Using high-precision control points, according to formula (1) ,
geometric distortion rectification is carried out on complex
images of homologous stereopair,then, calculate iteratively out
the six distortion parameters according to formula(7) in the
following :
a o =a o ' + da» ' + a 0 ‘~'daf' + b 0 ‘~'da 2
a { ‘ = af' +af'daf' + bf'da 2
a 2 = a 2 ' + a i 'dai ' + b 2 ‘ 'da 2
a 0 — b 0 + db 0 + a 0 db( + ò 0 db 2
a,' =6/ 1 +af'dbf l + bf'db 2
b 2 = b 2 "I - a 2 db x + db 2
Among them
Ì—1 I
a Q i a \ ’“2
7-1 _/-l Ì-1 »7-1 » 7-1 »7-1
5 Cl2 5 Oq 5 ¿U
i indicates iterative times,
0 ,l/ * ,i ' 2 is distortion parameter of the
preceding once, da 0 ,da x ,da 2 ,db 0 ,db x ,db 2 correc ^ on va i ue
of iterative calculation of this time.
3. INTERFEROGRAM PRODUCTION AND REMOVAL
OF THE PHASE OF FLAT EARTH
As we know, the single image’s phase of interferometry is of
little significance, phase difference between homologous image
points must be obtained, namely o = 7^(6^, — 6> 2 ), calculation
indicates O is in the range of [0,2x) ■
Because homologous complex images may be expressed as
follows:
m, =|w 1 |e ;01 = a, +bf,
it 2 = \u 2 \e j61 = a 2 + b 2 i
J°.2 * I
? j02 - |M 1 ||M 2 |e /(<?l 82}
= {a^a 2 + bf 2 ) + (a 2 b^ - af 2 )i
So A-
<f) = w(arctan[-
ct 2 b\ a f> 2
])
ct,ct n + b,b-
According to this principle, interferogram can be produced, and
its phase is fuzzy about 2ît, which is made up of two parts: the
phase component caused by terrain relative elevation, and that
caused by flat earth, when the elevation of two points on the
ground are the same, as figure(l) shows, phase difference
obtained in P V P 2 should be equal if there is no difference in
phase difference caused by flat earth, but the oblique distance
image-forming characteristic of INSAR results in phase
difference displacement of the two pointsP ]2 P 2 ■ Therefore,any
original interferogram needs subtracting phase difference ^
caused by effect of flat earth from original phase difference of
each point in the distance direction. Ultimately, the removal of
phase of flat earth finishes, thus, the achieved interferogram is
just the one corresponding to the topography.
And phase difference ^ is :
= 4;zn 5 Ar/(/l*r 0 *tan#)
n s is baseline distance component perpendicular to oblique
distance , oblique distance difference, T 0 the length of
oblique distance, and 0 the angle of incidence.
S2
Fig-(l)
According to satellite track parameters provided by European
Space Agency ,the satellite track attitude may be expressed as
linear function of time or low order polynomial, as the formula
(11) shows:
X = a n + a,t + aJ + aJ + a.t
(ID
Among them: X i s a coordinate (including X,Y,Z coordinate) of
satellite, and T is the time .
In general, the satellite track parameters include 0 X the angle
of incidence of short distance, 63 the one of long distance,
and 6 2 the one of middle point between 6 X and 0 3 in the
distance direction.so any angle of incidence 6 in image may
be expressed in formula (12):
6 = ay 2 +by + c
(12)
Among them: y is the ratio of row coordinate and the width of
the whole frame image, a,b,c is coefficient of fitting, the value
of a,b,c can be calculated by 0 V 6 2 ,0 2 \ Meanwhile, terrain
surface is fit by using several ground control points , like the
formula (13):
X = a 0 + a { x + a 2 y + a 3 xy + a 4 x 2 + a 5 y 2
(13)
Among them: X is the coordinate (including the coordinate
X, Y,Z ) of points on the ground, x is the column coordinate of
451