I don't think so.. Constitutive laws for shell composites normally are restricted to elastic relations. Consider that interlaminar stresses normally cause failure of composites and this is not well accounted for in classical lamination theory.

I don't know if you used the composite module present in Abaqus. But an another way is to describe the model in 2 parts : matrix and fibres. Next you can applied each constitutive law described in the software to each part.