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.
B I B L I O G R A F I A[1] Epperson E.H. Jr, Giroscopically Steerable Bullet, Patent USA, nr 4, 431, 150 appropriate by General Dynamic, Pamona, California, 14.02.1984.
[2] Koruba Z., Osiecki J.W., Budowa, dynamika i nawigacja pocisków rakietowych bliskiego zasięgu, cz. 1, skrypt nr 348, Politechnika Świętokrzyska, Kielce, 1999.
[3] Koruba Z., Osiecki J.W., Budowa, dynamika i nawigacja wybranych broni precyzyjnego rażenia, Podręcznik Akademicki, Politechnika Świętokrzyska, Kielce, 2006.
[4] Krzysztofik I., Osiecki J.W., Wykrywanie i śledzenie celów, skrypt nr 430, Politechnika Świętokrzyska, Kielce 2008.
[5] Grzyb M., Stefanski K., Numerical Simulation of Attack on the Non-maneuvering Target of Guided Bomb with Implemented Homing Algorithms, Computer Science in the Age of XXI Century, pp. 97-108, Technical University of Radom, 2012.
[6] Awrejcewicz J., Koruba Z., Classical mechanics.Applied mechanics and mechatronics, Advances in Mechanics and Mathematics, vol. 30, Monography, Springer 2012.
[7] Koruba Z., The Numerical analysis of dynamics and control of a gyroscopic scanning system in an anti-aircraft missile launcher, Journal of Communications in Nonlinear Science and Numerical Simulation, vol. 16, issue 5, pp. 2230-2236, 2011.
[8] Stefański K., Koruba Z., Analysis of the guiding of bombs an ground targets using a gyroscope system, Journal of Theoretical and Applied Mechanics, vol. 50, no. 4, pp. 967-973, 2012. 
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