Response of an Asymmetric Missile to Spin Varying through Resonance
Author:
Affiliation:
1. Ballistic Research Laboratories, Aberdeen Proving Ground, Md.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.50025
Reference14 articles.
1. Nonlinear motion of a missile with slight configurational asymmetries
2. Resonance instability for finned configurations having nonlinear aerodynamic properties
3. SOURCES, MECHANISMS AND CONTROL OF ROLL RESONANCE PHENOMENA FOR SOUNDING ROCKETS
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5. Chaos in Wraparound Fin Projectile Motion;Journal of Guidance, Control, and Dynamics;1998-03
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