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DEVELOPMENT OF A TACTICAL BALLISTIC MISSILE TRAJECTORY PREDICTION TOOL

Journal Name:

  • Istanbul University Journal of Electrical & Electronics Engineering

Publication Year:

  • 2005

Key Words:

Author Name
Abstract (2. Language): 
A trajectory prediction program was developed to predict the full trajectory (partially tracked by a satellite or a radar) of a tactical ballistic missile. In order to improve the accuracy of the ballistic coefficient an adaptive CD model is developed. Dynamic model, filtering of measurements, geocentric earth model and atmosphere model were applied and the details of the models and test results are presented. Input to the program is coordinates of the tracked trajectory portion and output is the full trajectory. In this way the launch and target point can be obtained within seconds of execution time.
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  • 2
1463-1467
  • English

REFERENCES

References: 

[1] Lee, S.C., Huang, C.Y., Liu, C.Y.,
“Trajectory Estimation for Tactical Ballistic
Missiles in Terminal Phase Using On-Line
Input Estimator”, Proc. Natl. Sci. Counc.
ROC(A), Vol. 23, No. 5, 1999, pp.644-653.
[2] Lee, S.C., Liu, C.Y., “Trajectory Estimation
of Reentry Vehicles by Use of On-Line Input
Estimator”, Journal of Guidance Control and
Dynamics, Vol. 22, No. 6, Nov.-Dec.
1999,pp.808-815.
[3] Crumpton, K.S., “The Effects of Filter and
Coordinate Frame Selection on the Accuracy
and Efficiency of Tactical Ballistic Missile
Parameter Estimation and Prediction”, Ph.D.
Thesis, University of Colorado, 2000.
[4] Robert M. Rogers, “Applied Mathematics in
Integrated Navigation Systems”, AIAA
Education Series.
[5] Buns, K. A., Stoy, S. L., Vukelich, S. R.,
“Missile DATCOM: User Manual – 1997
Fortran 90 Revision”, 1998.
[6] “U.S. Standard Atmosphere, 1976”, U.S.
Government Printing Office, Washington,
D.C., 1976.
[7] William H. Press, “Numerical Recipes”,
Cambridge University Press.

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