Nonlinear motion of a missile with slight configurational asymmetries
- 1 March 1971
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 8 (3) , 259-263
- https://doi.org/10.2514/3.30257
Abstract
No abstract availableKeywords
This publication has 8 references indexed in Scilit:
- ANALYSIS OF THE ANGULAR MOTION OF MISSILES.Published by Office of Scientific and Technical Information (OSTI) ,1970
- Nonlinear motion of a symmetric missile acted on by a double valued static moment.AIAA Journal, 1968
- Slender body estimates for two cubic aerodynamic damping moments.AIAA Journal, 1966
- Angular motion of a re-entering symmetric missileAIAA Journal, 1965
- Quasi-linear analysis of the nonlinear motion of a nonspinning symmetric missileZeitschrift für angewandte Mathematik und Physik, 1963
- FREE FLIGHT MOTION OF SYMMETRIC MISSILESPublished by Defense Technical Information Center (DTIC) ,1963
- The Prediction of Nonlinear Pitching and Yawing Motion of Symmetric MissilesJournal of the Aeronautical Sciences, 1957
- ON THE FREE FLIGHT MOTION OF MISSILES HAVING SLIGHT CONFIGURATIONAL ASYMMETRIESPublished by Defense Technical Information Center (DTIC) ,1953