Right option is (a) 1.02*(Wo^-0.06)*1.0
To elaborate: The design take-off gross weight is W0 = Wcrew + Wpayload + Wfuel + Wempty
The fuel and empty weight are taken as fractions of gross weight and thus following is given as
Empty weight fraction= Wempty / W0 = A*K*(W0) ^c
Where, A and c are constant and dependent of type of Aircraft and K = variable sweep constant
For a typical Jet transport aircraft with fixed sweep, A = 1.02, c = -0.06 and K = 1.0.