Roll-Axis Hydrofluidic Stability Augmentation System Development
Final rept. 29 Mar 1973-30 Sep 1974
HONEYWELL INC MINNEAPOLIS MN GOVERNMENT AND AERONAUTICAL PRODUCTS DIV
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The objective of this program was to develop, design, and flight test a roll-axis Hydrofluidic Stability Augmentation System HYSAS for the OH-58A helicopter. The system, when used with a yaw HYSAS, provides increased vehicle damping which improves the handling characteristics. Flight test evaluations were performed with satisfactory results.