Control power requirements are made up of stabilization and control of external disturbances, and basic maneuvering; stabilization required decreases with increasing design weight; maneuvering control required, however, is essentially independent of weight and may be installed in airplane as angular or as linear translation control; effect of gust environment on hovering VTOL transport is examined; factors to consider in control system design that affect performance and penalties associated with various control levels are outlined.
Control requirements and control methods for large V/STOL aircraft
SAE -- Paper
SAE Meeting ; 1965
1965
9 pages
Conference paper
English
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Control Requirements and Control Methods for Large V/STOL Aircraft
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