Zbigniew Koruba

Kielce University of Technology

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Izabela Krzysztofik

Kielce University of Technology

Daniel Gapiński

Kielce University of Technology

Zbigniew Dziopa

Kielce University of Technology

ŁN

Łukasz Nocoń

Kielce University of Technology

Piotr Szmidt

Kielce University of Technology

Jan Awrejcewicz

Lodz University of Technology

Marta Grzyb

Kielce University of Technology

J. Tuśnio

Kielce University of Technology

Konrad Stefański

Kielce University of Technology

Michał Sobolewski

Medical University of Silesia

Cooperative Institutions

Kielce University of Technology

Riga Technical University

Latvian Maritime Academy

Ventspils University of Applied Sciences

Polish Air Force Academy

Warsaw University of Technology

Latvian Environment, Geology and Meteorology Centre (Latvia)

Military University

National University "Yuri Kondratyuk Poltava Polytechnic"

Transport and Telecommunication Institute

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Dynamics and Control of the Gyroscopic Head used for the Laser Illumination of a Ground Target from the Quadcopter Deck

Communications - Scientific letters of the University of Zilina (2021)

Zbigniew Koruba Izabela Krzysztofik

In the paper authors investigate dynamics of a controlled quadcopter in terms of the possibility of its use for detection, observation, tracking and laser illuminating of both stationary and moving ground targets in the conditions of impact of random and kinematic excitations. The drone is equipped with a scanning and tracking Gyroscopic Head (GH) coupled with a laser target indicator. The drone is affected by random disturbances in the form of wind gusts or explosions of missiles. Kinematic excitations, such as drone maneuvers and vibrations from engines, act on the GH. This paper focuses mainly on control and stabilization of the gyroscopic head placed on the drone during the search, tracking and simultaneous laser illuminating of the target.

Quadcopter

Drone

Tracking (education)

10.26552/com.c.2021.2.b158-b164

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The numerical analysis of dynamics and control of a gyroscopic scanning system in an anti-aircraft missile launcher

Communications in Nonlinear Science and Numerical Simulation (2010)

Zbigniew Koruba

Dynamics

Interception

Missile Guidance

10.1016/j.cnsns.2010.04.041

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Citations (3)

Analysis of the guiding of bombs on ground targets using a gyroscope system

Journal of Theoretical and Applied Mechanics/Mechanika Teoretyczna i Stosowana (2012)

Konrad Stefański Zbigniew Koruba

This paper discusses the possibility of using a bomb flight control system in the form of a rapidly rotating heavy rotor jointly suspended in its body. Forced deflections of the rotor axis (gyroscope) in relation to the body axis generate torques, which change the direction of bomb flight and its guiding on the target. Some results of simulations are presented in a graphical form.

Helicopter rotor

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Citations (11)

Dynamics and Control of a Gyroscope-Stabilized Platform in a Ship Anti-Aircraft Rocket Missile Launcher

Diffusion and defect data, solid state data. Part B, Solid state phenomena/Solid state phenomena (2013)

Zbigniew Koruba

The paper presents the ways of stabilising and controlling a Ship Anti-Aircraft Rocket Missile Launcher (SAARML) with the use of a Three-Axis Gyroscope-Stabilized Platform (TAGSP). The analysis of the dynamics of the SAARML and TAGSP systems is conducted for the case of searching and tracking a manoeuvring air target in the conditions of interferences and the influence of kinematic forces from the base (ship's deck). Some research results are presented in a graphical form.

Rocket (weapon)

10.4028/www.scientific.net/ssp.196.124

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Citations (7)

The model of dynamics and control of modified optical scanning seeker in anti-aircraft rocket missile

Mechanical Systems and Signal Processing (2013)

Daniel Gapiński Zbigniew Koruba Izabela Krzysztofik

Rocket (weapon)

Missile Guidance

Tracking (education)

10.1016/j.ymssp.2013.11.016

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Citations (31)

Modelowanie i symulacja numeryczna samonaprowadzania pocisku rakietowego na cel naziemny z wykorzystaniem sterowanego giroskopu

Problems of Mechatronics Armament Aviation Safety Engineering (2014)

Edyta Ładyżyńska-Kozdraś Zbigniew Koruba

10.5604/20815891.1130218

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A process of gyroscope motion control in an autonomous system of target detection and tracking

Journal of Theoretical and Applied Mechanics/Mechanika Teoretyczna i Stosowana (1999)

Zbigniew Koruba

A control algorithm of a three-degree-of-freedom gyroscope axis motion emerging from a solution to the inverse problem of dynamic is presented in the paper. A complete system of non-linear differential equations represents the motion of axis of a gimballed gyroscope (i.e. mounted in the Cardan joint), including both the inertial parameters of all elements and resisting forces acting in joint bearings. The effect of the following factors: initial conditions choice, disturbances, as well as non-linearity, on precision of the gyro-axis required motion realisation is presented. Optimal parameters of the control algorithm correcting the gyro-axis motion are determined, as well.

Control moment gyroscope

Tracking (education)

Inverse dynamics

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Citations (2)

The dynamic model of a combat target homing system of an unmanned aerial vehicle

Journal of Theoretical and Applied Mechanics/Mechanika Teoretyczna i Stosowana (2010)

Zbigniew Koruba Edyta Ładyżyńska-Kozdraś

The work presents the concept of the application of an unmanned aerial vehicle (UAV) used in the process of direct reaching of ground targets (radio location stations, combat vehicles or even tanks). The kinematic model of UAV motion takes into consideration particular phases of the mission realised by the vessel, i.e. programmed flight during target search, follow flight after the encounter of the target as well as during the process of self directioning onto the target. Control laws for the automatic UAV combat pilot are presented and the dynamic model of automatically steered UAV is developed. In the examinations solutions of analytical mechanics for holonomic settings within the relative system tightly connected with the moving object are incorporated.

Homing (biology)

Holonomic

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Citations (9)

Analysis of Dynamics of Remote-Controlled Artillery-Missile System

Problems of Mechatronics Armament Aviation Safety Engineering (2018)

Zbigniew Koruba Piotr Szmidt Daniel Gapiński

The paper presents physical and mathematical model of the modified remote-controlled the artillery-missile system (AMS) system of the Wróbel II type that is intended to be located on a warship. The proposed system is used for independent detection, tracking and counteracting the means of air attack at short distances. Moreover, principle of operation of SAR is presented and analysis of the system’s dynamics was carried out. The results of investigations are given in a graphical form.

Artillery

Missile Guidance

Tracking (education)

Tracking system

Dynamics

10.5604/01.3001.0012.1102

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Citations (1)

Mechanizm zabezpieczająco-uzbrajający zapalnika do wyrobów rakietowych o ruchu obrotowym względem osi podłużnej

Zeszyty Naukowe Politechniki Świętokrzyskiej. Nauki Techniczne (2006)

J. Tuśnio Zbigniew Koruba

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