Obiekt

Tytuł odmienny:

Hybrydowy system sterowania bombą kierowaną w płaszczyźnie pionowej podczas samonaprowadzania w warunkach działania turbulencji ; Hybrydowy system sterowania bombą kierowaną w płaszczyźnie pionowej podczas samonaprowadzania w warunkach działania turbulencji

Współtwórca:

Marta GRZYB ; Marta GRZYB

Abstrakt:

The article presents a mathematical model and an algorithm for hybrid control of a bomb aimed at a moving ground target. The guided bomb flight control system subject to the study combines a conventional PD controller and a quasi-sliding mode (QSM) controller. The target trajectory was determined based on the kinematic relations of the mutual motion of the bomb and the ground target using the proportional approach method. The main aim of the article is to analyse the impact of atmospheric turbulence on the flight of a guided bomb, and then to determine its impact on homing parameters, such as homing time and accuracy of hitting a ground target. The numerical studies covered three types of controllers: conventional PID, quasi-sliding and hybrid. The effectiveness of the proposed control system was analysed without and during random atmospheric turbulence. The article examines the hybrid system’s properties for controlling guided bombs. Numerical studies were performed using the Matlab/Simulink software suite. The article presents selected results of this computer simulation.
; The article presents a mathematical model and an algorithm for hybrid control of a bomb aimed at a moving ground target. The guided bomb flight control system subject to the study combines a conventional PD controller and a quasi-sliding mode (QSM) controller. The target trajectory was determined based on the kinematic relations of the mutual motion of the bomb and the ground target using the proportional approach method. The main aim of the article is to analyse the impact of atmospheric turbulence on the flight of a guided bomb, and then to determine its impact on homing parameters, such as homing time and accuracy of hitting a ground target. The numerical studies covered three types of controllers: conventional PID, quasi-sliding and hybrid. The effectiveness of the proposed control system was analysed without and during random atmospheric turbulence. The article examines the hybrid system’s properties for controlling guided bombs. Numerical studies were performed using the Matlab/Simulink software suite. The article presents selected results of this computer simulation.

Miejsce wydania:

Warszawa
; Warszawa

Wydawca:

Wojskowa Akademia Techniczna ; Wojskowa Akademia Techniczna

Data utworzenia:

2010 r.0

Data złożenia:

2023-10-01 ; 2023-10-01

Data akceptacji:

2024-02-28 ; 2024-02-28

Data wydania:

2024-06-30 ; 2024-06-30

Rozmiar:

B5 ; B5

Identyfikator:

oai:ribes-88.man.poznan.pl:2701

Sygnatura:

doi:10.5604/01.3001.0054.6094 ; doi:10.5604/01.3001.0054.6094

ISSN elektroniczny:

2720-5266 ; 2720-5266

ISSN drukowany:

2081-5891 ; 2081-5891

Język:

angielski ; angielski

Licencja:

kliknij tutaj, żeby przejść ; kliknij tutaj, żeby przejść

Właściciel praw:

Wojskowa Akademia Techniczna ; Wojskowa Akademia Techniczna

Strona początkowa:

9 ; 9

Strona końcowa:

22 ; 22

Tom:

15 ; 15

Czasopismo:

PROMECH ; PROMECH

Słowa kluczowe:

guidance / homing, guided bomb, hybrid control system, sliding mode control, atmospheric turbulence ; guidance / homing, guided bomb, hybrid control system, sliding mode control, atmospheric turbulence