Modeling, PID Control and Simulation of a Rocket Launcher System

被引：0

作者：

Dokumaci, Korhan ^{[1
]}

Aydemir, M. Timur ^{[2
]}

Salamci, Metin U. ^{[1
]}

机构：

[1] Gazi Univ, Dept Mech Engn, Ankara, Turkey

[2] Gazi Univ, Elect & Elect Engn Dept, Ankara, Turkey

来源：

2014 16TH INTERNATIONAL POWER ELECTRONICS AND MOTION CONTROL CONFERENCE AND EXPOSITION (PEMC) | 2014年

关键词：

Rocket Launcher System; 2 DOF Manipulator; Electromechanical Actuating; Rocket Launcher Control;

D O I：

暂无

中图分类号：

TM [电工技术]; TN [电子技术、通信技术];

学科分类号：

0808 ; 0809 ;

摘要：

Rocket Launcher Systems are mechanisms that carry rockets and orient them to targets. A Rocket Launcher System (RLS) has two degrees of freedom; it rotates about -z and -y axes to provide azimuth (yaw) and elevation (pitch) angles respectively. Azimuth and elevation axes are actuated by servo motors and a set of gears. The aim of the control for the RLS is to attain the elevation and azimuth angles with desired speeds and also, if salvo firings (periodic firings with constant time interval) are needed, to keep azimuth and elevation axes on the target. This paper first develops the mathematical model of the Launcher System, and then presents control applications for the launcher with simulations. In the simulations, salvo firing model is applied to launcher to disturb positioning and the responses of the controller to firing disturbances are obtained.

引用

页码：1283 / 1288

页数：6

共 50 条

[41] Control system of Brazilian Launcher
Leite, WD
4TH ESA INTERNATIONAL CONFERENCE ON SPACECRAFT GUIDANCE, NAVIGATION AND CONTROL SYSTEMS AND TUTORIAL ON MODERN AND ROBUST CONTROL: THEORY, TOOLS AND APPLICATIONS, 2000, 425 : 401 - 405
[42] Design, Modeling and Simulation of PID Control for DC/AC Inverters
Blachuta, Marian
Rymarski, Zbigniew
Bieda, Robert
Bernacki, Krzysztof
Grygiel, Rafal
2019 24TH INTERNATIONAL CONFERENCE ON METHODS AND MODELS IN AUTOMATION AND ROBOTICS (MMAR), 2019, : 428 - 433
[43] Optimal sliding mode servo control with integral term for rocket launcher
Zhu, Yu-Chuan
Ma, Da-Wei
Li, Zhi-Gang
Le, Gui-Gao
Binggong Xuebao/Acta Armamentarii, 2007, 28 (10): : 1272 - 1275
[44] Simulation Research of PID Control System Based on Simulink
Chen, Gui Xu
Song, Hong
Geng, Qing Hua
PROCEEDINGS OF THE SECOND INTERNATIONAL CONFERENCE ON MODELLING AND SIMULATION (ICMS2009), VOL 1, 2009, : 133 - 138
[45] Simulation of power system based on PID excitation control
Xu H.
Yin S.
1600, Italian Association of Chemical Engineering - AIDIC (59): : 835 - 840
[46] Modeling and verification of a missile launcher system
Isik, C.
Ider, S. K.
Acar, B.
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART K-JOURNAL OF MULTI-BODY DYNAMICS, 2014, 228 (01) : 100 - 107
[47] Development of Loading Training System Based on Software Mode for Rocket Launcher
Yang Qingwen
Fang Shidong
Yang Guang
Tong Decheng
Wu Shuo
ICCSE 2008: PROCEEDINGS OF THE THIRD INTERNATIONAL CONFERENCE ON COMPUTER SCIENCE & EDUCATION, 2008, : 1019 - 1022
[48] Lightweight of pedestal of vehicle-carried multiple rocket launcher system
Lin, Guo-Wen
Ma, Da-Wei
Zhu, Sun-Ke
Dandao Xuebao/Journal of Ballistics, 2012, 24 (02): : 101 - 105
[49] Fuzzy fault diagnosing for the transmission system of some multiple rocket launcher
Wang Shuhai
Feng Mingzhi
Tao Xia
ISTM/2007: 7TH INTERNATIONAL SYMPOSIUM ON TEST AND MEASUREMENT, VOLS 1-7, CONFERENCE PROCEEDINGS, 2007, : 2733 - 2735
[50] Linear active disturbance rejection control for two-axis coupling position servo system of rocket launcher
Zheng, Ying
Ma, Da-Wei
Yao, Jian-Yong
Hu, Jian
Binggong Xuebao/Acta Armamentarii, 2015, 36 (06): : 987 - 993

← 1 2 3 4 5 →