Publikacje

Abstract:

The work considers the effect of the kinematic action resulting from the basic motion of the vehicle on the dynamics of the launcher and the gyroscope acting as the drive of the opto-electro-mechanical target coordinator in a self-guided missile. The problem was analyzed using a hypothetical short-range anti-aircraft system. The simulation results were represented graphically.

B I B L I O G R A F I A[1] Z. Koruba, “Dynamics and control of a gyroscope on board of
an flying object”, in Monographs, Studies, Dissertations, vol.
25, Kielce University of Technology, Kielce, 2001, (in Polish).
[2] Z. Dziopa, Z. Koruba, and I. Krzysztofik, “ An analysis of the
dynamics of a launcher-missile system on a moveable base”, in
Monographs, Studies, Dissertations, vol. 34, Kielce University
of Technology, Kielce, 2010, (in Polish).
[3] I. Krzysztofik and J. Osiecki, Detection and Tracking of Targets, Scientific Issue of Kielce University of Technology, vol. 32, No. 430, Kielce, 2008.
[4] Z. Dziopa, “The modelling and investigation of the dynamic properties of the sel-propelled anti-aircraft system, Monographs, Studies, Dissertations vol. 32, No. M9, Kielce University
of Technology, Kielce, 2008.
[5] V.P. Mishin, Missile Dynamics, Mashinostroyeniye, Moscow, 1990.
[6] V.A. Svietlitskiy, Dynamics Start Flying Objects, Nauka, Moscow, 1963

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An analysis of the gyroscope dynamics of an anti-aircraft missile launched from a mobile platform