Subroutine CMA_DEF

Defines a set of elements that are affected by a change in attitude.

Calling convention:

call cma_def( grp, cma_id, ierr)
Arguments Data type Input/Output Description
grp Char*(*) Input Long group name of elements that are affected by attitude change. Typically this will be the outside of a spacecraft.
cma_id integer Output Internal id of cma definition
ierr integer Output Error flag. Zero means no error, other values TBD.

Typically only the exterior elements are selected for the attitude change. If there are no moving elements in the interior, all conductances will remain unchanged, which is equivalent to the interior elements tracking the motion of the exterior.