MISSILE COMMAND - A REAL TIME MISSILE SYSTEM WITH EMBEDDED GUIDANCE CONTROL USING DIJKSTRA'S ALGORITHM

被引：0

作者：

Arun, R. ^{[1
]}

Sriram, M. ^{[1
]}

机构：

[1] Velammal Engn Coll, Madras 18, Tamil Nadu, India

来源：

ICIAS 2007: INTERNATIONAL CONFERENCE ON INTELLIGENT & ADVANCED SYSTEMS, VOLS 1-3, PROCEEDINGS | 2007年

关键词：

D O I：

暂无

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

This paper deals with the design of a Real Time Missile System embedded with Shortest Path Algorithm concept, which helps for its guidance. The specialty of this paper is that each missile will have their own radar and can be completely automatic i.e. "the power to think on its own". Every missile launched will hit the target with 100% certainty. In the missile system we use the "Key Concepts".

引用

页码：1368 / 1373

页数：6

共 50 条

[1] Geometric analysis of flight control command for tactical missile guidance
Kuo, CY
Soetanto, D
Chiou, YC
IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY, 2001, 9 (02) : 234 - 243
[2] Traffic system path guidance algorithm based on missile guidance
Gong, Yan
Li, Su-Jian
Xing, En-Hui
Jiaotong Yunshu Xitong Gongcheng Yu Xinxi/Journal of Transportation Systems Engineering and Information Technology, 2014, 14 (04): : 180 - 185
[3] Simulation of Control and Guidance System for the Spinning Missile
Meng Daikui (China Changfeng System Engineering Corporation
Chinese Journal of Systems Engineering and Electronics, 1994, (03) : 49 - 56
[4] Application of Genetic Algorithm on Missile Fire Allocation and Command Control
Feng, Jie
Yao, Hai-Tao
International Conference on Mechanics, Building Material and Civil Engineering (MBMCE 2015), 2015, : 81 - 86
[5] Time-delay control for integrated missile guidance and control
Park B.-G.
Kim T.-H.
Tahk M.-J.
International Journal of Aeronautical and Space Sciences, 2011, 12 (03) : 260 - 265
[6] FUZZY GUIDANCE LAW FOR SURFACE-TO-AIR MISSILE IN THE COMMAND CONTROL SYSTEMS
Trung-Dung Pham
Qui Tran
Duc-Vuong Vu
2012 INTERNATIONAL CONFERENCE ON CONTROL, AUTOMATION AND INFORMATION SCIENCES (ICCAIS), 2012, : 317 - 322
[7] An integrated design for missile guidance/control/tracking system
Xu Yefeng
Qiu Haitao
SEVENTH INTERNATIONAL SYMPOSIUM ON INSTRUMENTATION AND CONTROL TECHNOLOGY: OPTOELECTRONIC TECHNOLOGY AND INSTUMENTS, CONTROL THEORY AND AUTOMATION, AND SPACE EXPLORATION, 2008, 7129
[8] Sliding Mode Control for Integrated Missile Guidance and Control System
Xiong, Yu
Guo, Jianguo
Zhou, Jun
PROCEEDINGS OF THE 38TH CHINESE CONTROL CONFERENCE (CCC), 2019, : 8371 - 8374
[9] Least-time path algorithm based on missile guidance
Gong, Yan
Li, Sujian
Xing, Enhui
Journal of Transportation Systems Engineering and Information Technology, 2013, 13 (06) : 94 - 100
[10] Integrated guidance and control of missile's with θ-D method
Xin, Ming
Balakrishnan, S. N.
Ohlmeyer, Ernest J.
IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY, 2006, 14 (06) : 981 - 992

← 1 2 3 4 5 →