lay
ISK
sor
IIT
TM data processing software
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TM data processing software consists of four stages, which
are designated as pass 0, pass 1
tively( See Fig.2 ).
stage are presented in the following.
(1)^pass^0
Pass O is for
reproducing HDT recorded
with satellite image
data and feeding the
image data, calibration
data, Dl restore dala
and PCD(payload
correction data)
disk memories.
into
Using ephemeris
data which are telexed
from NASA , compute
satellite orbit infor-
mation and determine
HDT reading start
time. Next,feed PCD
into a disk memory as
they are reproduced
with real time speed,
and then feed image
data, calibration
data as they reproduced
with 1/16 speed.
Histogram data which
are generated by TMCE
( TM control equipment)
are also stored at the
same time in two RM
disks.
(2) pass I
Geometric Correction
Radiometric Correction
pass 2 and pass 3 respec-
General descriptions of each processing
Pass © Pass 1 — Pass 2/3
Image
Image Data
Data
Ephemeris & i
E | iEphemeris
Atti tude Computation
Component
- T attitude] Uu
onputati |
fengutstio]: 3
d
= ere Low Freq. /
ne tude + Comment | Resampling
rConputation along scan
eee = ; Look up |"i
Table | ——
Scan | | : Resampling
1 Profile Min & Low] |. ross scan
Distortion i
Correction
Ferd Cal. Data Res i
ampling
Generation ECC RR s
*
| | Histgram '
Modification Gain &
- Offset
L | i
Standard +
Deviation Look up
Table
Pass Q —————— Pass |
— Pass 2/3
Fig. 2 Flow chart of geometric & radiometric correction
Pass 1 computes radiometric and geometric correction co-
efficients for removing distortions due to sensor re
sponsivity
characteristics and satellite attitude changes and outputting
the image data by designated mapping projection method.
Satellite position, velocity and at
the edited. PCD data;
titude are computed from
In case of missing ephemeris data points,
the missing data are interpolated with adjacent data points
by the VINTI's ephemeris generation method.