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Motion of the two-control airplane in rectilinear flight after initial disturbances with introduction of controls following an exponential lawAn airplane in steady rectilinear flight was assumed to experience an initial disturbance in rolling or yawing velocity. The equations of motion were solved to see if it was possible to hasten recovery of a stable airplane or to secure recovery of an unstable airplane by the application of a single lateral control following an exponential law. The sample computations indicate that, for initial disturbances complex in character, it would be difficult to secure correlation with any type of exponential control. The possibility is visualized that the two-control operation may seriously impair the ability to hasten recovery or counteract instability.
Document ID
19930081383
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Klemin, Alexander (New York University)
Date Acquired
September 6, 2013
Publication Date
September 1, 1937
Report/Patent Number
NACA-TN-615
Accession Number
93R10673
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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