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The analog work performed included the six-degree-of-freedom hover simulation; the longitudinal three-degree-of-freedom transition simulation; the longitudinal three-degree-of-freedom conversion simulation, the six-degree-of-freedom perturbation conventional flight simulation, and the simulation of gas generator control for wing-fan thrust. Supporting analyses included roll-yaw coupling and structural feedback in the pitch mode. Further work accomplished involved the stability augmentation system specification; the development of the bridge concept for roll and yaw louver control; support of various hardware tests; the generation of the specification for the DeFlorez point light source visual display; furnishing consolation services during the DeFlorez display installation and testing, and developing the yaw, roll and pitch direction cosine relationships.