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Analytical Method of Approximating the Motion of a Spinning Vehicle with Variable Mass and Inertia Properties Acted Upon by Several Disturbing ParametersAn analytical method has been developed which approximates the dispersion of a spinning symmetrical body in a vacuum, with time-varying mass and inertia characteristics, under the action of several external disturbances-initial pitching rate, thrust misalignment, and dynamic unbalance. The ratio of the roll inertia to the pitch or yaw inertia is assumed constant. Spin was found to be very effective in reducing the dispersion due to an initial pitch rate or thrust misalignment, but was completely Ineffective in reducing the dispersion of a dynamically unbalanced body.
Document ID
19980228448
Acquisition Source
Langley Research Center
Document Type
Other - NASA Technical Report (TR)
Authors
Buglia, James J.
(NASA Langley Research Center Hampton, VA United States)
Young, George R.
(NASA Langley Research Center Hampton, VA United States)
Timmons, Jesse D.
(NASA Langley Research Center Hampton, VA United States)
Brinkworth, Helen S.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1961
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-TR-R-110
Report Number: NASA-TR-R-110
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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