Very light airplane longitudinal dynamic stability analysis
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 1 October 2002
Abstract
A linearized analytic model of general longitudinal movement of airplane is discussed. Linearized deviation equations of motion, derived in stability axes system, are applied to the parametric analysis of airplane's longitudinal dynamic stability under arbitrary symmetric flight conditions. The analytic model is generated in the form of interactive software package PODYST_ALFA. This is used to show the influence of some constructional and mass parameters on the longitudinal airplane motions after encountering disturbance for a chosen steady level flight.
Keywords
Citation
Danek, V. (2002), "Very light airplane longitudinal dynamic stability analysis", Aircraft Engineering and Aerospace Technology, Vol. 74 No. 5, pp. 425-430. https://doi.org/10.1108/00022660210442263
Publisher
:MCB UP Ltd
Copyright © 2002, MCB UP Limited