Nonlinear motion of a missile with slight configurational asymmetries
Author:
Affiliation:
1. Ballistic Research Laboratories, Aberdeen Proving Ground, Md.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.30257
Reference13 articles.
1. The Prediction of Nonlinear Pitching and Yawing Motion of Symmetric Missiles
2. Quasi-linear analysis of the nonlinear motion of a nonspinning symmetric missile
3. Angular motion of a re-entering symmetric missile
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