Transactions of the Korean Society of Mechanical Engineers A (대한기계학회논문집A)

The Korean Society of Mechanical Engineers (대한기계학회)
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A Development of Numerical Analysis Software on Dynamic Analysis for Lunching System

발사 시스템의 동역학 해석을 위한 수치해석 프로그램 개발

  • Published : 2008.12.01
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Abstract

In the initial stage of guided missile launching, the dynamic stability of a missile is highly influenced by disturbances from the outside and interferences among the launching system parts. This research develops a program for guided missile launching system analysis. Random variables are used to analyze quantitatively the missile characteristic response. An example of results with the program applied into a specific System is presented to demonstrate the effectiveness of the propose method.

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References

  1. Chin, S. S., 1961, “Missile Configuration Design,” McGRAW-HILLBOOK Company.Inc.
  2. Edward I. Haug, 1989, “Computer Aided Kinematics and Dynamics of Mechanical System,” Allay and Bacon
  3. Johnson, K. L., 1985, “Contact Mechanics,” Cambridge University Press
  4. Lee, C. W., 1984, ”Dynamic Modeling and Analysis of MRLS,” ADD
  5. Yoo, W. S. and Lee. B. H, 1993, “A Study of CAE for Launching System,” Guided Missile conference, pp. 551-557
  6. Lim, B. S., Jeon, H. S., Kim, J. H. and Sim, W. J., 1993, “Early Movement Analysis of the Guided Launching Missile,” Guided Missile Conference, pp. 621-628
  7. Ahn, J. S. and Lim. B. S., 2001, ”Flexible MultiBody Dynamic Analysis of Missile Behavior for initial Launching,” ADAMS User Conference
  8. Ahn, J. S. and Lim. B. S., 2002, “A Statistical Approaching Method of the Guided Missile Movement Launching on the Ship,” RecurDyn User Conference
  9. Cho, H. J, Bae, D. S., Choi, J. H. and Ahn, J. S., 2003, ”Dynamics Analysis of Launch System Using Probabilistic Variables,” Guided Missile conference
  10. Hunt, K.H. and Crossley, F.R.E., 1975, Coeffient of Restitution Interpreted as Damping in Vibroimpact. ASME Journal of Applied Mechanics, 97:440-445, June