NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Minimum control power for VTOL aircraft stability augmentationVTOL aircraft stability augmentation system design based on control theory state variable methods, using minimum power levels
Document ID
19700054740
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Swaim, R. L.
Date Acquired
August 5, 2013
Publication Date
June 1, 1970
Subject Category
Aircraft
Accession Number
70A30856
Funding Number(s)
CONTRACT_GRANT: NGR-15-005-009
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.

Related Records

There are no records associated with this record.
No Preview Available