Translational rate command (TRC) in helicopter flight involves controlling the earth-referenced forward and side velocities, using the helicopter’s cyclic control. Handling qualities requirements for TRC systems suggest that the design should comprise an inner attitude command-attitude hold (ACAH) loop, with TRC control as an outer loop. This forms a non-square system, and a method to determine the implications of this structure for stability robustness is proposed here. Control synthesis was performed using the method of individual channel analysis and design. This technique is a neo-classical, frequency-domain control analysis and design method for multivariable systems. The control law obtained is very simple, and the handling qualities, assessed by non-linear simulation, are predicted to be at ‘Level 1’ (satisfactory without improvement). The conditions for stability robustness are satisfied at frequencies of significance for the handling qualities.