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Feasibility analysis of the modified point mass trajectory model for the need of ground artillery fire control systems

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Języki publikacji
EN
Abstrakty
EN
The work shows computational results of the effect of a simplified mathematical model of the flight dynamics of a spin-stabilized projectile on the accuracy and speed of calculation parameters for the projectile trajectory (in the entire range of operating quadrant elevation of the barrel and possible perturbations of the conditions firing) to determine an appropriate mathematical model for the automated fire control systems of ground artillery.
Rocznik
Strony
511--522
Opis fizyczny
Bibliogr. 11 poz., rys.
Twórcy
  • Military University of Technology, Faculty of Mechatronics and Aerospace, Warsaw, Poland
Bibliografia
  • 1. Baranowski L., 2011, Modeling, Identification and Numerical Study of the Flight Dynamics of Ballistic Objects for the Need of Field Artillery Fire Control Systems, Military University of Technology, Warsaw, p. 258 [in Polish]
  • 2. Carlucci D.E., Jacobson S.S., 2008, Ballistics: Theory and Design of Guns and Ammunition, CRC Press, Taylor & Francis Group
  • 3. Gacek J., 1997, Exterior Ballistics. Part I. Modeling Exterior Ballistics and Flight Dynamics, Military University of Technology, Warsaw, p. 352 [in Polish]
  • 4. Koruba Z., Dziopa Z., Krzysztofik I., 2010, Dynamics of a controlled anti-aircraft missile launcher mounted on a moveable base, Journal of Theoretical and Applied Mechanics, 48, 2, 279-295
  • 5. Kowaleczko G., Żyluk A., 2009, Influence of atmospheric turbulence on bomb release, Journal of Theoretical and Applied Mechanics, 47, 1, 69-90
  • 6. Lieske R.F., Reiter M.L., 1966, Equations of Motion for a Modified Point Mass Trajectory, Memorandum Report No. 1314, U.S. Army Ballistic Research Laboratory, Aberdeen Proving Ground
  • 7. Ładyżyńska-Kozdraś E., Koruba Z., 2012, Model of the final section of navigation of a selfguided missile steered by a gyroscope, Journal of Theoretical and Applied Mechanics, 50, 2, 473-485
  • 8. McCoy R.L., 1999, Modern Exterior Ballistics. The Launch and Flight Dynamics of Symmetric Projectiles, Schiffer Publishing
  • 9. Procedures to Determine the Fire Control Inputs for use in Indirect Fire Control Systems, STANAG 4144 (Ed. 2), 2005
  • 10. The ISO Standard Atmosphere, ISO 2533, 1975
  • 11. The Modified Point Mass and Five Degrees of Freedom Trajectory Models, STANAG 4355 (Ed. 3), 2009
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-a30fcc47-9973-4171-87c1-acfda4d5081d
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