Autor: Kowaleczko, M. - Katalog OPAC zbiorów

Skocz do pozycji: 1.

Tytuł:: Estimation of the accuracy of laser guided bomb
Autorzy:: Kowaleczko, G.
Pietraszek, M.
Powiązania:: https://bibliotekanauki.pl/articles/244869.pdf
Data publikacji:: 2016
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: exterior ballistics
guided munitions
flight control
Opis:: The main goal of the bomb release is to hit the target with a maximum accuracy. Therefore, special active control systems are utilized to improve this accuracy. Some of the most popular are semi-active laser systems of guidance. Selected target is pointed with high-intensity laser by an airborne or ground laser designator. The laser-guided bomb (LGB) tracks this target using on-board laser seeker and adjusts its trajectory. The main task of the control system is to steer the bomb in the way allowing fixing the reflected laser beam in the centre of photo sensor array. This keeps the bomb axis straight toward the target. The aim of this study is to identify factors influencing on the accuracy of the LGB. It was performed for the prototype of LGB, which was designed in the Air Force Institute of Technology. This is the modernized version of the classical LB-10M bomb. Originally, this bomb has only four rear stabilizers and it has been equipped with four additional fins (Fig. 1). These fins allow controlling the bomb's path in active way. Earlier studies have shown that this is the useful method of bomb control both in longitudinal and lateral motions. Analysis proved that range of the bomb can be effectively changed. This paper presents method of flight simulations for released LGB. Calculations were performed using sixdegrees- of-freedom mathematical model of the LB-10M bomb motion. Aerodynamics was calculated using commercial software. Control laws were determined based on signals detected by two pairs of laser sensors. Exemplary results of simulations are submitted and conclusions focused on the main factors influencing on bombing accuracy are shown.
Źródło:: Journal of KONES; 2016, 23, 3; 271-279
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 2.

Tytuł:: Model dynamiki zrzutu bomby w warunkach turbulencji
Model of bomb airdrop dynamics at turbulence conditions
Autorzy:: Kowaleczko, G.
Pietraszek, M.
Grajewski, K.
Powiązania:: https://bibliotekanauki.pl/articles/235862.pdf
Data publikacji:: 2018
Wydawca:: Wojskowy Instytut Techniczny Uzbrojenia
Tematy:: bomba korygowana
symulacja numeryczna
turbulencja atmosferyczna
model dynamiki lotu
guided bomb
numerical simulation
turbulence of the atmosphere
fight dynamics model
Opis:: Celem niniejszego artykułu jest przedstawienie częściowych wyników badań symulacyjnych prowadzonych aktualnie w Instytucie Technicznym Wojsk Lotniczych. Badania te dotyczą dynamiki lotu ćwiczebnej bomby lotniczej LBĆw-10, która została opracowana w ITWL, a obecnie podlega modernizacji. Symulacje wykonano wykorzystując autorskie oprogramowanie opracowane na potrzeby tych badań. W artykule przedstawiono klasyczny model ruchu przestrzennego bomby oraz podano podstawowe dane tego obiektu. Dokładnie opisano sposób obliczania oddziaływań aerodynamicznych uzupełniając ten opis o przykładowe charakterystyki aerodynamiczne, które otrzymano wykorzystując komercyjne oprogramowanie PRODAS. Dodatkowo przedstawiono sposób uwzględnienia zmienności pola wiatru, a w szczególności turbulencji atmosfery. Zastosowano stochastyczny model pola wiatru. Pokazano przykładowe wyniki obliczeń, które zostaną wykorzystane w procesie modernizacji bomby polegającym na wprowadzeniu aktywnego sterowania torem lotu.
The purpose of this article is to present partial results of simulation tests currently conducted at the Air Force Institute of Technology. These tests concern the flight dynamics of the LBCw-10 flight bomb, which was developed at ITWL and is currently undergoing modernization. Simulations were carried out using proprietary software developed for the needs of these studies. The article presents a classic model of spatial motion of a bomb and basic data of this object. The method of calculating aerodynamic forces is described in detail, complementing this description with exemplary aerodynamic characteristics, which were obtained using commercial PRODAS software. Additionally, the method of taking into account the variability of the wind field, and in particular the turbulence of the atmosphere is presented. A stochastic wind field model was used. Illustrative results of calculations are shown, which will be used in the process of bomb modernization involving the use of active flight path control.
Źródło:: Problemy Techniki Uzbrojenia; 2018, 47, 146; 119-143
1230-3801
Pojawia się w:: Problemy Techniki Uzbrojenia
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 3.

Tytuł:: Influence of geometric characteristics of the bomb-fluger system on its dynamics
Autorzy:: Kowaleczko, G.
Pietraszek, M.
Klemba, T.
Powiązania:: https://bibliotekanauki.pl/articles/241709.pdf
Data publikacji:: 2018
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: guided bombs
bomb-fluger system
aerodynamics simulations
Opis:: The article presents the results of numerical simulations of the bomb-fluger system drop. This system consists of two rigid bodies – a bomb and a fluger, which are connected by a biaxial joint. For the analysis, an author's program was used to simulate the bomb-fluger system drop. Influence of the characteristic points of the system on its stability and dynamics was investigated. Particularly, locations of a bomb mass centre, a fluger mounting point, a fluger aerodynamic focus were tested. The article presents a model of the examined bomb in the wind tunnel, characteristic points of a bomb-fluger system, waveforms of values rate of change angles and the values of angles for different distances, waveforms of values of the angle of nutation and the pitch angle of the fluger relative to the bomb, diagrams of examined points of the location of the centre of the mass and pressure of the fluger, waveforms of values rate of change angles and the values of these angles for different locations of the centre of the mass of the fluger, waveforms of values of the angle of nutation and the pitch angle of the fluger relative to the bomb for different locations.
Źródło:: Journal of KONES; 2018, 25, 4; 155-163
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 4.

Tytuł:: The evaluation of the efficiency of active control system for aerial bomb
Autorzy:: Kowaleczko, G.
Żyluk, A.
Pietraszek, M.
Wijaszka, M.
Powiązania:: https://bibliotekanauki.pl/articles/244285.pdf
Data publikacji:: 2018
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: simulation
PID controller
laser-guided bombs
Opis:: The article presents the results of numerical simulation of a laser-guided bomb, which is dropped in calm weather conditions. The prototype of such a bomb was developed at the Air Force Institute of Technology. It was a result of the modification process of the classical training bomb. The modification consisted of building on the bomb's board a detection system to track targets that are designated by laser and a control system to adjust bomb’s glide path to precisely strike the target. In the simulation research, geometric and mass characteristics of the classical training bomb were used. Aerodynamic characteristics of the bomb have been determined using commercial software PRODAS. Using the mathematical model of the bomb spatial motion and model of the laser detection system series of simulations were performed. The main goal was to determine the effectiveness of the adopted construction solution. Therefore, simulations were performed for various initial positions of the bomb and fixed position of the target. It allowed finding the set of control laws coefficients giving the most accuracy of the bomb. The influence of structural modifications of the detection system on the possibility of effective detection and location of the target was also investigated. In the article, exemplary results of numerical calculations performed with the author's software are also shown.
Źródło:: Journal of KONES; 2018, 25, 4; 165-174
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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Skocz do pozycji: 5.

Tytuł:: Evaluation of the possibility of bomb flight control
Autorzy:: Kowaleczko, G.
Olejniczak, E.
Pietraszek, M.
Żyluk, A.
Powiązania:: https://bibliotekanauki.pl/articles/245642.pdf
Data publikacji:: 2015
Wydawca:: Instytut Techniczny Wojsk Lotniczych
Tematy:: airborne munitions
bomb flight
active bomb control
aerodynamic bomb
PRODAS calculations
Opis:: This paper presents theoretical model dedicated to a guided bomb. A mathematical description of the six-degrees-of-freedom motion of the bomb is shown. Particular attention was paid on aerodynamic forces and moments generated by additional control fins mounted on the front part of the bomb. Exemplary results of a numerical simulation of bombing are submitted and conclusions focused on the possibility of flightpath control are formulated. The paper concerns on the equations of bomb spatial motion and kinematic relations expressed making use of moving coordinate systems, the common origin of which is located at the centre of mass of the bomb. The set of equations of the rotating motion about the centre of mass in the body-fixed reference frame is presented. Aerodynamic forces and moments acting on the bomb are described. Coefficients are determined using the PRODAS software with detailed geometry of the LB-10M bomb. The coefficients were determined for different Mach numbers from 0.4 to 0.8. The important task was research investigations of aerodynamic characteristics with a wind tunnel and a set of experiments in real bombing conditions.
Źródło:: Journal of KONES; 2015, 22, 3; 105-115
1231-4005
2354-0133
Pojawia się w:: Journal of KONES
Dostawca treści:: Biblioteka Nauki

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