Abstract:
this paper presents on the stability analysis for
RAVAN twin boom H-Tail Medium Scale UAV which has been
developed by University of Moratuwa. It is required to
understand the UAV behavior for the small perturbations in high
altitudes while it is flying to be invisible. Indeed, without doing a
proper stability analysis in different flying conditions, there is a
high risk to fail the UAV for perturbations. Not only that but also
it will help to optimize aerodynamic behavior for prolonging the
flight endurance and effective deployment. The proper stability
analysis will facilitate to increase the control flexibility.XFLR5
computational fluid dynamic software is used to do this stability
analysis.
