Dergiler / Istanbul University Journal of Electrical and Electronics Engineering / 2005 / Cilt: 5 - Sayı: 2

Development of a tactical ballistic missile trajectory prediction tool

Sayfa
1463–1467
Yayın Tarihi
2022-10-18
DOI
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⚡ TL;DR(1 Cümlede Hızlı Çıkarım)

In this way the launch and target point can be obtained within seconds of execution time.

📌 3 Maddede Bu Makale

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Amaç & Hipotez:A trajectory prediction program was developed to predict the full trajectory (partially tracked by a satellite or a radar) of a tactical ballistic missile.
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Temel Bulgular & Veri:In order to improve the accuracy of the ballistic coefficient an adaptive CD model is developed.
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Sonuç & Katkı:In this way the launch and target point can be obtained within seconds of execution time.
🔬Tür:Modelleme & Sayısal Simülasyon
📍Kapsam:Genişletilmiş Akademik Örneklem
⚙️Değişkenler:Alan Parametreleri

Abstract

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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Bu Makaleye Atıf Yap

KARASOY, S., AKGÜL, A. (2022). Development of a tactical ballistic missile trajectory prediction tool. Istanbul University Journal of Electrical and Electronics Engineering, Cilt: 5 - Sayı: 2, 1463–1467. https://ajindex.com/articles/543856

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Kaynakça (6)

  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
  6. William H. Press, “Numerical Recipes”, Cambridge University Press.