Problems exporting part CoG wrt assembly Datum

[Anonymous]

Hi,

I have been trying to customise an iLogic rule to give me the centre of gravity of '1st level' parts and sub-assemblies within an assembly file. I have managed to export everything I wanted to an excel file, but it turns out that this program is exporting the centre of mass of each individual component with respect to it's own datum, rather than the position of it's centre of gavity with respect to the assembly datum.

I have attached the rule to this post. Any help would be greatly appreciated.

Cheers!