Efficient Orbit Integration by Linear Transformation for ...

3 downloads 0 Views 378KB Size Report
variables to be integrated is increased to 16 per celestial body, the new method provides the best performance among the manifold correction methods we devel ...
Æ                          

                  

   

!

"

 !

 

#$#

  % &  !!  ' !   (  ! )  *

 + ) ,*+( .   !! (   ! !     )  )!    /  

(         '        ! ! (      (  0 1  (    

)    ) !    /       ) &        

 !!    

!  )      (  !2  )

 !

!     !3   (  )!           !    *+ ( .    (   0  !    ) 

)        '  

!   0 

  !     ' !   (  !               &  

 ( !   !! !       )    !    ! !      )     (  0    !           

 ' !   (  !0  (    )       ( !    !  4     !    ! !   )

  ( 

)!    !  ! ! )  *+( .!     0   

        

#5#

  

  !      ! 

.  ! !    )    )!  *

 + ) ,*+- ( .  ,*

 

! + ) 64)  ! !  0       *+ ( .   

   ! 

.   ! )     !  !Æ  )        7            (   !      (  '!  0 8 )   )  (         !   (   '  )    

(  !  !            

  !(   

 )   *+ ( .  )  ! !   .    0 + (  ) 9  8:  !     ) ;