Flight Motion of a Continuously Elastic Finned Missile

The motion of elastic finned projectiles has been analyzed by various approximate theories. The correct equations of small-amplitude motion are derived for a symmetric missile. The aerodynamic and elastic symmetries are used to allow the use of complex variables to describe the lateral motion in a n...

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Veröffentlicht in:	Journal of guidance, control, and dynamics control, and dynamics, 2003-01, Vol.26 (1), p.89-98
Hauptverfasser:	Murphy, Charles H, Mermagen, William H
Format:	Artikel
Sprache:	eng
Schlagworte:	Boundary conditions Complex variables Computation Coordinates Cross-disciplinary physics: materials science rheology Damping Drag coefficients Dynamics and kinematics of a particle and a system of particles Exact sciences and technology Fineness Fineness ratio Finned projectiles Free vibration Fundamentals and general Induced drag Ordinary differential equations Partial differential equations Particle dynamics Physics Rheology Symmetry Velocity Yaw
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