the 
5 
mes 
20 
es 
20 
mes 
20 
es 
uency 
od by 
1t and 
ion of 
r.13(a) 
      
   
(a) output of an CCD (b) TDI output. 
Fig.8 TDI at eight times when the satellite has attitude fluctuation around the roll axis. 
  
REP 
(c) TDI output with correction 
  
  
  
(a) output of an CCD (b) TDI output (c) TDI output with correction 
  
   
Fig.9 TDI at eight times when the satellite has attitude fluctuation around roll and pitch axis at the 
same time. 
(a) TDI output (b) TDI output 
Fig.10 TDI at thirty-two times when satellite has attitude fluctuation around the roll axis. 
       
(a) TDI output (b) TDI output 
Fig.11 TDI at sixty-two times when satellite has attitude fluctuation around roll axis. 
International Archives of Photogrammetry and Remote Sensing. Vol. XXXII, Part 7, Budapest, 1998 
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