Application of the Modified Material Point Method in Calculating the Parameters of Flight

Izdanje: Sinteza 2016 - International Scientific Conference on ICT and E-Business Related Research

DOI: 10.15308/Sinteza-2016-230-236

Link: https://doi.org/10.15308/Sinteza-2016-230-236

Apstrakt:
The aim of this study was to analyze the effect of structural characteristics and initial conditions on foreign ballistic missile features a classic. The problem is interesting because it extends the resolution of physical models of classical projectile motion that describes a translational movement. Applying software solutions proposed by the authors to save resources and reduce time numerical calculations as designing modern technical systems requires the use of simple physical and mathematical models and software that provide the required accuracy. Use of this software solution is in line with trends in the development of modern solutions in the external ballistics. This model allows the numerical integration of the equations for a shorter time than the model with six degrees of freedom.
Ključne reči: modified material point, force, torque, coefficients, rotate, body

Preuzimanje citata:

BibTeX format
@article{article,
  author  = {D. Regodić, D. Jerković, A. Jevremović and R. Regodić}, 
  title   = {Application of the Modified Material Point Method in Calculating the Parameters of Flight},
  journal = {Sinteza 2016 - International Scientific Conference on ICT and E-Business Related Research},
  year    = 2016,
  doi     = {10.15308/Sinteza-2016-230-236}
}
RefWorks Tagged format
RT Conference Proceedings
A1 Dušan Regodić
A1 Damir Jerković
A1 Aleksandar Jevremović
A1 Radomir Regodić
T1 Application of the Modified Material Point Method in Calculating the Parameters of Flight
AD International Scientific Conference Sinteza, Beograd, Srbija
YR 2016
NO doi: 10.15308/Sinteza-2016-230-236
Unapred formatirani prikaz citata
D. Regodić, D. Jerković, A. Jevremović and R. Regodić, Application of the Modified Material Point Method in Calculating the Parameters of Flight, International Scientific Conference Sinteza, 2016, doi:10.15308/Sinteza-2016-230-236