PRELIMINARY SYSTEMS ANALYSIS AND SIMULATION
GENERAL ELECTRIC CO CINCINNATI OH ADVANCED ENGINE AND TECHNOLOGY DEPT
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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.
- Research and Experimental Aircraft