Comparison of Effectiveness of Antiaircraft Missile Homing Controlled by Rotary Executive System
Journal Title: Problemy Mechatroniki. Uzbrojenie, lotnictwo, inżynieria bezpieczeństwa - Year 2013, Vol 4, Issue 4
Abstract
In this paper, the numerical comparative analysis of antiaircraft missile homing was carried out. The controlling of this missile flight was realized by means of rotor made of high density material, jointly mounted inside of missile airframe. The rotor accelerated to high rotational speed takes features of gyroscope, therefore change of its axis location with reference to longitudinal axis of missile causes that missile changes its flight direction. Comparison of homing was carried out for two algorithms, and some of simulations results were presented graphically.
Authors and Affiliations
Konrad STEFAŃSKI, Marta GRZYB
Keywords
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