PRE-PROGRAMMED FLIGHT PATH OF AIR-TO-GROUND MISSILE

被引：0

作者：

Grzyb, M. ^{[1
]}

Koruba, Z. ^{[1
]}

机构：

[1] Kielce Univ Technol, Dept Appl Comp Sci & Armament Engn, Fac Mechatron & Mech Engn, AlejaTysiacelcia Panstwa Polskiego 7, PL-25314 Kielce, Poland

来源：

ENGINEERING MECHANICS 2018 PROCEEDINGS, VOL 24 | 2018年

关键词：

missile; pre-programmed trajectory; guidance; control; dynamics; DYNAMICS;

D O I：

10.21495/91-8-261

中图分类号：

TH [机械、仪表工业];

学科分类号：

0802 ;

摘要：

The paper reports a control algorithm for air-to-ground missile that performs a pre-programmed flight along an ellipse section. The control system of the object flight is based on classical PD controllers. The efficiency of the system that guides the missile onto a ground target was analysed. The paper presents selected results of numerical simulations obtained using Matlab/Simulink package.

引用

页码：261 / 264

页数：4

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