International Journal of Aerospace Engineering / 2019 / Article / Tab 3

Research Article

Flight Dynamics Modeling and Dynamic Stability Analysis of Tilt-Rotor Aircraft

Table 3

Airplane mode eigenvalue validation.

Hover modeNatural modeCalculatedReference [20]GTRS

LongitudinalPhugoid
Short-period pitch
LateralDutch roll
Spiral subsidence-0.1384-0.0497-0.1226
Roll subsidence-0.7128-0.9378-1.0649

We are committed to sharing findings related to COVID-19 as quickly and safely as possible. Any author submitting a COVID-19 paper should notify us at help@hindawi.com to ensure their research is fast-tracked and made available on a preprint server as soon as possible. We will be providing unlimited waivers of publication charges for accepted articles related to COVID-19. Sign up here as a reviewer to help fast-track new submissions.