Compute the eigenvalues and eigenvectors of the two systems

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Reference no: EM132164919

Linear models for the Boeing 747 are:

Longitudinal dynamics at Mach 0.8 and 20,000 ft

1606_Lateral dynamics.jpg

Nomenclature: u body- x velocity, w body- y velocity, q pitch rate, θ pitch angle

Lateral dynamics at Mach 0.8 and 40,000 ft

1072_Longitudinal dynamics.jpg

Nomenclature: β sideslip angle, r yaw rate, p roll rate, Φ roll angle.

1. Use MATLAB to compute the eigenvalues and eigenvectors of the two systems.

Are they stable? Try to describe physically the individual modes.

2. Are the two systems controllable?

Reference no: EM132164919

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