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Modern Geomatics Technologies and Applications

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             In Figure 5 the GRACE and GRACE-FO mission the signals are between [-1.5, 2.5]⁡× 10 . In the
         Cartwheel  mission  the  signals  are  between  [-3.5,  3.5]⁡× 10 −3 .  The  pendulum  mission’s  signals  are
                                 −3
                                                                                           −3
         between [-1.5, 1.5]⁡× 10 . The Helix scenario’s signals are between [-5.5, 6.5]⁡× 10 .
             If the strike angle could be 90 degrees, then the maximum variations will be along the meridian and
         will almost match the satellites’ flight path. Therefore, the missions will sense much more signals rather
         than  the  earlier  position.  Figure  5  confirmed  this.  In  this  situation,  the  sharp  signals  are  not  seen  in
         Cartwheel, Pendulum and Helix scenarios, too.

             5.  Conclusions

             In the future, satellite missions should be able to solve much more problems in the gravity field. The
         GRACE mission gave us good results as the first experience. But its observations have only along-track
         signals;  therefore,  it  seems  that  because  of  the  satellite  motion,  a  large  part  of  signals  is  inevitably
         removed. If our formations involve a cross-track or radial components, they should have the same features
         as a GRACE-type leader-follower configuration. In the best situation, if observations include at least either
         of  cross-track  or  along-track  together  with  a  radial  one,  the  results  will  noticeably  improve.  The
         observations in such formations are significantly richer in gravitational content. This condition is not of
         course limited to coseismic signals detection.
             Despite the high power signal strength in Cartwheel, Pendulum and Helix, the sensitivity to coseismic
         in  this  case  study,  is  much  lower  than  GRACE  and  GRACE_FO.  Perhaps  one  of  the  most  important
         factors is to reduce the distance between two satellites. This distance is changing drastically in cartwheel,
         Pendulum and Helix but has little change in GRACE and GRACE-FO. However, it should be noted that,
         the  wide  distance  between  Grace  and  Grace-FO  always  exist.  In  conclusion,  the  coseismic  signals
         sensitivity strongly depends on the distance between satellites. This factor is one of the major factors that
         lead to the above mentioned results.

             .

         References


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                9.1) from inversion of GRACE gravity data. Earth and Planetary Science Letters, 335, 72-79.
         CASE,  K.,  KRUIZINGA,  G.,  WU,  S.  2002.  GRACE  level  1B  data  product  user  handbook.  JPL
                Publication D-22027.
         CHANG, E. T., CHAO, B. F. 2011. Coseismic surface deformation of the 2011 off the Pacific coast of
                Tohoku  Earthquake:  Spatio-temporal  EOF  analysis  of  GPS  data.  Earth,  planets  and  space,  63,
                649-654.
         CHEN,  J.,  WILSON,  C.,  TAPLEY,  B.,  GRAND,  S.  2007.  GRACE  detects  coseismic  and  postseismic
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         DAI,  C.,  SHUM,  C.,  WANG,  R.,  WANG,  L.,  GUO,  J.,  SHANG,  K.,  TAPLEY,  B.  2014.  Improved
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