Zbigniew Dziopa

Modelling and the Elements of Controlled Dynamics of the Anti-Aircraft Missile Launcher Based Onboard the Warship

The paper presents a physical and mathematical model of the controlled anti-aircraft launcher based onboard the ship, whose aim is to fight low-flying air targets. Selected tests results of the computer simulation are presented in a graphic form.

Analysis of Results of Empirical Investigations of Launcher–Missile System Using TEMA Motion Program Environment

The paper presents an analysis of the pictures, recorded from the testing ground investigations, obtained with application of the fast-digital camera Phantom v9.1. The analysis was focused on determination of the kinematics of motion of the launcher-missile system. TEMA Motion program was used for motion analysis of the investigated system. The courses of variability of kinematic values characterising motion of the selected points of the launcher were determined. The results analysis showed that the launcher undergoes the linear displacement (X, Y) and angular one () that cause significant differences in the flight trajectory of the successively launched missiles.

Empirical research of human-weapon system

Abstract Rapid firing of the Skorpion vz.61 machine gun was registered at a police shooting range. The shooting was executed by a policeman from the secret service. The registration was done with the use of a fast digital camera Phantom v9.1 together with the necessary equipment. With the use of the specialised TEMA software, which serves to analyse the recorded image, the courses of the variation of kinematic quantities characterizing the weapon movement were obtained. On the basis of the courses of the variation of the displacement, velocity and acceleration over time, the behaviour of the machine gun in thirteen characteristic points of its operation was specified.

Elements of Dynamics Analysis of the Warship Launcher of Anti-Aircraft Short Range Homing Missiles

The paper presents a physical and mathematical model of a short range missile launcher based onboard a warship. The conducted numerical simulation allowed for developing an analysis of the anti-aircraft assembly dynamics. The selected responses of the system are demonstrated in the form of physical values characterizing the launcher motion.