Research On Missile System With Strapdown Guidance Technology

被引：1
|
作者：
Feng, Delong [1 ]
Yang, Suochang [1 ]
Liu, Yingxi [2 ]
机构：
[1] Shijiazhuang Mech Engn Coll, Dept Missilery Engn, Shijiazhuang, Peoples R China
[2] Xidian Univ, Natl Key Lab Sci & Technol Radar Signal Proc, Xian, Peoples R China
来源：
CURRENT TRENDS IN THE DEVELOPMENT OF INDUSTRY, PTS 1 AND 2 | 2013年 / 785-786卷
关键词：
proportional guidance law; guided missile; strapdown; seeker;
D O I：
10.4028/www.scientific.net/AMR.785-786.1560
中图分类号：
T [工业技术];
学科分类号：
08 ;
摘要：
This paper presents a project of missile guidance system based on the strapdown guidance technology. The project is composed of strapdown seeker and inertial measurement unit. The integrated guidance and control technology have been adopted. The project raise accuracy of missiles on the premise that the low cost should be guaranteed. According to simulation experiment, this paper proves the feasiblity of the scheme, and it has good ballistic missile.
引用
收藏
页码：1560 / +
页数：2
相关论文
共 50 条
  • [31] New Kalman filter design for strapdown homing guidance system
    Song, J.-M. (sjm318@bit.edu.cn), 2005, Beijing Institute of Technology (25):
  • [32] Strapdown inertial guidance system consisting of piezoelectric inertial sensors
    Zhao, Zhong
    Yadian Yu Shengguang/Piezoelectrics and Acoustooptics, 2000, 22 (02): : 78 - 80
  • [33] Research on target tracking technologies to a guidance radar of anti-missile weapon system
    Sun, Qing
    Ji, Jun Liang
    Sun, Yong
    INFORMATION TECHNOLOGY AND COMPUTER APPLICATION ENGINEERING, 2014, : 377 - 380
  • [34] Research on target acquisition requirements to a guidance radar of anti-missile weapon system
    Sun, Qing
    Tao, Jian Feng
    Ji, Jun Liang
    INFORMATION TECHNOLOGY AND COMPUTER APPLICATION ENGINEERING, 2014, : 373 - 376
  • [35] Advanced missile guidance with hybrid system models
    Cong, S
    Hong, L
    Chen, GS
    PROCEEDINGS OF THE 37TH IEEE CONFERENCE ON DECISION AND CONTROL, VOLS 1-4, 1998, : 4714 - 4719
  • [36] A New Simulation Technology Research for Missile Control System based on DSP
    Tian, Bin
    Yu, Jianqiao
    Mei, Yuesong
    PROCEEDINGS OF THE 3RD INTERNATIONAL CONFERENCE ON MATERIAL, MECHANICAL AND MANUFACTURING ENGINEERING, 2015, 27 : 678 - 685
  • [37] STANDARD MISSILE: GUIDANCE SYSTEM DEVELOPMENT.
    Witte, Robert W.
    McDonald, Robert L.
    Johns Hopkins APL Technical Digest (Applied Physics Laboratory), 1981, 2 (04): : 289 - 298
  • [38] 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
  • [39] STRAPDOWN GUIDANCE ERROR ANALYSIS
    MORTENSEN, RE
    IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 1974, AE10 (04) : 451 - 457
  • [40] Research of Integrated Guidance and Control for Missile in Pitch Channel
    Zhao, Xueling
    Guo, Limei
    2018 EIGHTH INTERNATIONAL CONFERENCE ON INSTRUMENTATION AND MEASUREMENT, COMPUTER, COMMUNICATION AND CONTROL (IMCCC 2018), 2018, : 1373 - 1377
12345