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2 Missile Trajectory Models, Aerodynamic Derivatives, Dynamic Coefficients and
Missile Trajectory Models, Aerodynamic Derivatives,
Missile Trajectory Models 9
Missile Trajectory Models 11 Define the following variables: V-missile body velocity; V; θ-missile flight path angle; γV -missile symmetrical plane deflection angle; , #, γ-missiles yaw angle, pitch angle, roll angle; α, β-angle of attack, angle of sideslip; Vx, Vy, Vz-velocity component (earth coordinate system); Vxb, Vyb, Vzb-velocity component (missile body coordinate system); !
Missile Trajectory Models 13
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