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.