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
Space shuttle pilot-induced-oscillation research testingThe simulation requirements for investigation of pilot-induced-oscillation (PIO) characteristics during the landing phase are discussed. Orbiters simulations and F-8 digital fly-by-wire aircraft tests are addressed.
Document ID
19840012498
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Powers, B. G. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 4, 2013
Publication Date
February 1, 1984
Subject Category
Aircraft Stability And Control
Report/Patent Number
NAS 1.15:86034
H-1227
NASA-TM-86034
Report Number: NAS 1.15:86034
Report Number: H-1227
Report Number: NASA-TM-86034
Accession Number
84N20566
Funding Number(s)
PROJECT: RTOP 505-34-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

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