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The linearized longitudinal Equations of motion of a typical
Business jet in steady level flight is given by the following
equation: (8u 8w 89 80) = (-0.00643 -0.0991 -0.000222 0
0.0263 -0.629 -0.00153 0 0 820 -0.668 1 -32.2 0 0 0) (8u 8w
89 80) Use MATLAB to find the eigenvalues and
eigenvectors of the system matrix A above. A wind gust
causes a perturbation of delta theta = 1 degree in steady
level flight. Find the response of the airplane to this
perturbation using a modal analysis.
Solution

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The linearized longitudinal Equations of motion of a typical Business jet in steady level flight is given by the following equation: (8u 8w 89 80) = (-0.00643 -0.0991 -0.000222 0 0.0263 -0.629 -0.00153 0 0 820 -0.668 1 -32.2 0 0 0) (8u 8w 89 80) Use MATLAB to find the eigenvalues and eigenvectors of the system matrix A above. A wind gust causes a perturbation of delta theta = 1 degree in steady level flight. Find the response of the airplane to this perturbation using a modal analysis. Solution Name: Description: ...
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