The Analysis of Trajectory of 122 mm Rotary Missile under the Influence of Interferences

Abstract

In this paper the analysis of influence on trajectory of 122 mm unguided rotary missile has been presented. Results of interferences that act during the flight of unguided missile are his dispersion in the form of range and lateral deflections. The influence of deviation of thrust has been researched by means of computer simulation. Results of analysis and research work have been presented in the form of graphs and charts.

Authors and Affiliations

Bogdan MACHOWSKI, Krzysztof MOTYL, Konrad SIENICKI

Keywords

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  • EP ID EP62922
  • DOI -
  • Views 109
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How To Cite

Bogdan MACHOWSKI, Krzysztof MOTYL, Konrad SIENICKI (2011). The Analysis of Trajectory of 122 mm Rotary Missile under the Influence of Interferences. Problemy Mechatroniki. Uzbrojenie, lotnictwo, inżynieria bezpieczeństwa, 2(4), 97-112. https://europub.co.uk/articles/-A-62922