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[108320] Artykuł:

The Remote Control of the Artillery Rocket Set as a Strongly Nonlinear System Subject to Random Loads

Czasopismo: Electronics   Tom: 10, Zeszyt: 1507, Strony: 1-17
ISSN:  2079-9292
Opublikowano: Czerwiec 2021
 
  Autorzy / Redaktorzy / Twórcy
Imię i nazwisko Wydział Katedra Do oświadczenia
nr 3
Grupa
przynależności
Dyscyplina
naukowa
Procent
udziału
Liczba
punktów
do oceny pracownika
Liczba
punktów wg
kryteriów ewaluacji
Zbigniew Koruba orcid logo WMiBMKatedra Technik Komputerowych i Uzbrojenia**Takzaliczony do "N"Inżynieria mechaniczna50100.00100.00  
Piotr Szmidt orcid logo WMiBMKatedra Technik Komputerowych i Uzbrojenia**Takzaliczony do "N"Automatyka, elektronika, elektrotechnika i technologie kosmiczne50100.00100.00  

Grupa MNiSW:  Publikacja w czasopismach wymienionych w wykazie ministra MNiSzW (część A)
Punkty MNiSW: 100


DOI LogoDOI    
Keywords:

control  nonlinear system dynamics  linearization  target tracking  Kalman filter 



Abstract:

On the modern battlefield, fighting capabilities,such as speed, target detection range, target identification capabilities, and shooting effectiveness, of short-range artilleryrocket sets(ARSs) are constantly being improved. Problems arise when attempting tosuccessfully fire such kits in the face of disruption from both the cannon and the moving platform on which the cannon is mounted. Furthermore, the set is a variable mass system since it can fire anywhere from a few to dozens or even hundreds of missiles in a brief period of time, implying that theARSisa highly nonlinear system of variable parameters (non-stationary). Thiswork shows how to control such asystem. If the ARS is placed on a moving basis where there is bothasystem and measurement noise, the state variables must be restored,and the ARS data must be filtered. Therefore, in addition to the LQR regulator, anextended Kalman filter was used. As a consequence of this synthesis, anLQG (linearquadraticGaussian) regulator of ARS was obtained, which was used to follow the target along the line of sight. The key goal of this paper is to develop control algorithms that will increase the performance of ARS control in elevation and azimuth, as well as the accuracy of achieving and eliminating maneuverable air targets. Moreover, through the quality criterion adopted,we hope toaffect control energy costs while maintaining control precision. Graphical representations of certain computational simulation results are provided.