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Derivation and definition of a linear aircraft modelA linear aircraft model for a rigid aircraft of constant mass flying over a flat, nonrotating earth is derived and defined. The derivation makes no assumptions of reference trajectory or vehicle symmetry. The linear system equations are derived and evaluated along a general trajectory and include both aircraft dynamics and observation variables.
Document ID
19890005752
Document Type
Other - NASA Reference Publication (RP)
Authors
Duke, Eugene L. (NASA Hugh L. Dryden Flight Research Center Edwards, CA, United States)
Antoniewicz, Robert F. (NASA Hugh L. Dryden Flight Research Center Edwards, CA, United States)
Krambeer, Keith D. (NASA Hugh L. Dryden Flight Research Center Edwards, CA, United States)
Date Acquired
September 5, 2013
Publication Date
August 1, 1988
Subject Category
AIRCRAFT STABILITY AND CONTROL
Report/Patent Number
NASA-RP-1207
NAS 1.61:1207
H-1391
Funding Number(s)
PROJECT: RTOP 505-66-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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