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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
/
2021
/
Article
/
Tab 3
/
Research Article
The Investigation on
Adaptive Control of the Tilt-Rotor Aircraft
Table 3
Airplane mode (
)
eigenvalues validation.
Hover mode
Natural mode
Calculated
GTRS
Longitudinal
Phugoid
Short-period pitch
Lateral
Dutch roll
Spiral subsidence
-0.1384
-0.1226
Roll subsidence
-0.7128
-1.0649