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
Qualitative Simulator Study of Longitudinal Stick Forces and Displacements Desirable During TrackingIn this study in which an airplane simulator with one degree of freedom (pitch) was used, results were determined for three conditions of airplane dynamics. For an undamped natural frequency of 1/2 cps with a damping ratio of 0.18 and for an undamped natural frequency of 1 cps with a damping ratio of 0.11, moderate longitudinal stick forces and displacements were desired.
Document ID
19930085061
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Faber, Stanley
Date Acquired
August 16, 2013
Publication Date
February 1, 1958
Report/Patent Number
NACA-TN-4202
Report Number: NACA-TN-4202
Accession Number
93R14351
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
CONTROL, LONGITUDINAL
STABILITY, LONGITUDINAL - DYNAMIC
PILOTING TECHNIQUES

Related Records

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