Publikacje

Abstract:

The analysis focuses on the dynamics of a hypothetical anti-aircraft system during the missile launch. The results of the computer simulation of motion of the launcher-missile system are represented graphically. The diagrams provide information about the range of kinematic excitations acting on the opto-electro-mechanical coordinator of the target in a self-guided missile.

B I B L I O G R A F I A1. Z. Dziopa, "The dynamics of a rocket launcher placed on a self-propelled vehicle", Mechanical Engineering 81 (3), 23-30 (2004).
2. Z. Dziopa, "The missile coordinator system as one of the objects of an anti-aircraft system", 6th Int. Conf. on Armament Technology: Scientific Aspects of Armament Technology, Military University of Technology 1, 221-229 (2006).
3. V. A. Svietlitskiy, Dynamics Start Flying Objects, Nauka, Moscow, 1963.
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. Z. Koruba, Z. Dziopa, and I. Krzysztofik, "Dynamics and control of a gyroscope-stabilized platform in a self-propelled antiaircraft system", J. Theoretical and Applied Mechanics 48 (1), 5-26 (2010).

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An analysis of the dynamics of a launcher-missile system on a moveable base