NASA NTRS · 19700054740
Minimum control power for VTOL aircraft stability augmentation
Abstract
VTOL aircraft stability augmentation system design based on control theory state variable methods, using minimum power levels
Keep this discovery
Explore connections, maps & timelines
Swaim, R. L.. 1970-06-01. Minimum control power for VTOL aircraft stability augmentation. https://ntrs.nasa.gov/citations/19700054740
Cite the original work for its findings. Save a collection to share your selection of sources.