Dynamics and Control of Gyroscopic System of Bomb Guidance on a Ground Target
Journal Title: Problemy Mechatroniki. Uzbrojenie, lotnictwo, inżynieria bezpieczeństwa - Year 2015, Vol 6, Issue 2
Abstract
The paper presents an algorithm of guiding the bomb on a ground target using the gyro system. There are considered different cases of the execution of flight path program combined with bomb homing in the final stretch of the flight. There are also quoted some of the results of computer simulation.
Authors and Affiliations
Zbigniew KORUBA, Marta GRZYB
Keywords
Related Articles
- EP ID EP63058
- DOI -
- Views 66
- Downloads 0
Analysis of Operation of a Driving Band Mounting in a Projectile’s Shell
The paper presents computational modelling using the Finite Element Method (FEM) for technological operation of a driving band mounted in a groove of a projectile shell. Exemplary results of analysis for shrapnel cal. 3...
Odrzut hamowany w obiekcie specjalnym kalibru 7,62 mm z tłumikiem magnetoreologicznym TR-1.0M
Przedmiotem pracy jest próba poznania wpływu wprowadzenia do układu broń ramienna – strzelec, systemu programowania przebiegu zjawiska odrzutu poprzez zastosowanie sterowanego tłumika magnetoreologicznego (MR). Przedstaw...
Chosen Issues of Military Radar Protection Against Antiradiation Missiles
The paper deals with the concept of suppression of enemy air defence with antiradiation missiles (ARM). ARM performance metrics and parameters are presented and compared. Some Anti-ARM techniques are discussed, i.e. low...
Numerical Analysis of Operation Process of Gas Piston System with Slide for the Assault Rifle of Modular Small Arms System Cal. 5,56 mm
The aim of the paper is to present the possibility of using the numerical analysis to describe the operation process of system the gas piston with the slide for the assault rifle of modular small arms system cal. 5,56 mm...
Estimation of Loads Acting on Flaps of the Su-22 Aircraft for Fatigue Tests
The paper presents the results of the calculation of forces acting on the flaps of the Su-22 aircraft during take-off and landing. Four different analytic and experimental calculation methods were used to increase the re...