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Linear models for the Boeing 747 are:
Longitudinal dynamics at Mach 0.8 and 20,000 ft
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
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?
It is given that a- iron has a BCC crystal structure, an atomic radius R = 0.124 nm, and atomic weight AFe = 55.85 g/mol. Calculate the following quantities for a- iron: Lattice parameter. Total number of atoms in the unit cell. Volume of the unit ce..
measure the velocity of air. If the deflection deflection (the vertical distance between the fluid levels in the two arms) is 7.3 cm, determine the air velocity. Take the density of air to be 1.25 kg/m3.
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