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Modelling and the elements of controlled dynamics of the anti-aircraft missile launcher based onboard the warship

机译：基于军舰的防空导弹发射器建模及其动力学控制要素

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The paper presents a physical and mathematical model of the controlled anti-aircraft launcher based onboard a ship, whose aim is to fight low-flying air targets. Selected tests results of the computer simulation are presented in a graphic form.

机译：本文提出了一种基于舰载受控防空发射器的物理和数学模型，其目的是打击低空飞行的目标。计算机模拟的选定测试结果以图形形式显示。

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来源
《Mechatronic systems, mechanics and materials》|2011年|p.269-280|共12页
会议地点 Jastrzebia Gora(PL)
作者
Zbigniew DZIOPA; Zbigniew KORUBA;
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作者单位

Kielce University of Technology, Faculty of Mechatronics and Machine Building, Kielce, Poland;

Kielce University of Technology, Faculty of Mechatronics and Machine Building, Kielce, Poland;

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会议组织
原文格式 PDF
正文语种 eng
中图分类工程材料一般性问题;
关键词
dynamics and control; anti-aircraft; missile launcher;

机译：动态和控制；防空;导弹发射器;

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专利

1. Modelling and the elements of controlled dynamics of the anti-aircraft missile launcher based onboard the warship [J] . Dziopa Z., Koruba Z. Diffusion and Defect Data. Solid State Data, Part B. Solid State Phenomena . 2012,第Null期

机译：舰载防空导弹发射器的建模及其动力学控制要素
2. Elements of dynamics analysis of the warship launcher of anti-aircraft short range homing missiles [J] . Dziopa Z. Diffusion and Defect Data. Solid State Data, Part B. Solid State Phenomena . 2013,第Null期

机译：防空短程寻的导弹的舰载发射器动力学分析要素
3. DYNAMICS OF A CONTROLLED ANTI-AIRCRAFT MISSILE LAUNCHER MOUNTED ON A MOVEABLE BASE [J] . Zbigniew Koruba, Zbigniew Dziopa, Izabela Krzysztofik Journal of teoretical and applied mechanics . 2010,第2期

机译：可移动基座上安装的可控反飞机导弹发射器的动力学
4. Modelling and the elements of controlled dynamics of the anti-aircraft missile launcher based onboard the warship [C] . Zbigniew DZIOPA, Zbigniew KORUBA Special Session on Mechatronic Systems, Mechanics and Materials . 2012

机译：基于军舰的防空导弹发射器控制动态的建模与元素
5. Dynamic model based state estimation in a heavy duty diesel aftertreatment system for onboard diagnostics and controls [D] . Surenahalli, Harsha S. 2013

机译：重型柴油后处理系统中基于动态模型的状态估计，用于车载诊断和控制
6. Modeling and Simulation of Control Actuation System with Fuzzy-PID Logic Controlled Brushless Motor Drives for Missiles Glider Applications [O] . Murali Muniraj, Ramaswamy Arulmozhiyal 2015

机译：模糊PID逻辑控制的无刷电机驱动控制系统的建模与仿真
7. Adaptive control of anti-aircraft missile launcher mounted on a mobile base [O] . Krzysztofik Izabela, Koruba Zbigniew 2012

机译：安装在活动基座上的防空导弹发射器的自适应控制
8. The wind-induced loads on a dynamically scaled model of a large missile in launching position [R] . Buell, D. A., Kenyon, G. C. 1959

机译：在发射位置的大型导弹的动态缩放模型上的风致载荷

Modelling and the elements of controlled dynamics of the anti-aircraft missile launcher based onboard the warship

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