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- W154069609 abstract "Changes in angle of attack in system were sensed indirectly by gages which responded to strains induced in wing structure. Output signals were amplified, filtered, and used to activate swashplate actuators. System provided significant reduction in blade loads and desirable changes in hub forces and moments." @default.
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- W154069609 date "1974-09-01" @default.
- W154069609 modified "2023-09-23" @default.
- W154069609 title "Swashplate feedback control for tilt-rotor aircraft" @default.
- W154069609 hasPublicationYear "1974" @default.
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