Research of Missile Parameterized Design System with ProToolkit

被引：0
|
作者：
Zhao, H. Z. [1 ]
Yin, F. L. [1 ]
机构：
[1] Shenyang Ligong Univ, Coll Equipment Engn, Shenyang 110159, Peoples R China
来源：
DIGITAL DESIGN AND MANUFACTURING TECHNOLOGY II | 2011年 / 215卷
关键词：
Missiles; Secondary development; Pro/Toolkit; Parameterized Design;
D O I：
10.4028/www.scientific.net/AMR.215.393
中图分类号：
TH [机械、仪表工业];
学科分类号：
0802 ;
摘要：
The system structure of missile parameterized design is put forward to solve the repeat problems in the process of designing and manufacturing missiles. It is illustrated that in Pro/E environment the combination of missile design parameters with constraint relation is adopted to develop missile parameterized system with VC++6.0 and Pro/Toolkit used as secondary development tools for the secondary development and through the dynamic linkage, and the missile parameterized design system is integrated with Pro/E tightly. The missiles designers can obtain series of projectiles or new types of projectiles by modifying main design parameters, which making it possible to meet with a certain standard tactically and technically and shorten the cycle of designing new products.
引用
收藏
页码：393 / 396
页数：4
相关论文
共 50 条
  • [41] Research on the Missile Ballistic System Simulation Based on Matlab
    Kong, Fancheng
    Chen, Wei
    Zhang, Di
    Bai, Zhenzhou
    PROCEEDINGS OF THE 2017 INTERNATIONAL CONFERENCE ON ELECTRONIC INDUSTRY AND AUTOMATION (EIA 2017), 2017, 145 : 1 - 4
  • [42] Research on Penetration Technology of Intelligent Cluster Missile System
    Liu Zongang
    Lu Jiaguo
    Dong Zhen
    2019 INTERNATIONAL CONFERENCE ON ROBOTS & INTELLIGENT SYSTEM (ICRIS 2019), 2019, : 245 - 249
  • [43] Research on entities' model of missile in general CGF system
    Deng, JJ
    Li, YB
    Zhang, L
    ISTM/2005: 6th International Symposium on Test and Measurement, Vols 1-9, Conference Proceedings, 2005, : 6889 - 6892
  • [44] Test Technology Research on Missile Infrared System Range
    Shi Sheng-bing
    Wang Chang-an
    Wang Guang-wei
    2016 2ND INTERNATIONAL CONFERENCE ON MECHANICAL, ELECTRONIC AND INFORMATION TECHNOLOGY ENGINEERING (ICMITE 2016), 2016, : 218 - 222
  • [45] On variable structure design of missile electromechanical servo system
    Jun, Zhou, 1600, (08):
  • [46] Preliminary design of a hybrid propulsion multimission missile system
    Sims, JD
    Frederick, RA
    JOURNAL OF SPACECRAFT AND ROCKETS, 1997, 34 (02) : 186 - 191
  • [47] Overload Control System Design of a Deflectable Nose Missile
    Sun Xiaofeng
    Gu Liangxian
    Gong Chunlin
    CEIS 2011, 2011, 15
  • [48] Design of the Teaching Demonstration Platform of Missile Control System
    Yang, Tao
    Chang, Xiaofei
    Fu, Wenxing
    Yan, Jie
    SYSTEM SIMULATION AND SCIENTIFIC COMPUTING, PT II, 2012, 327 : 153 - 159
  • [49] Design and Implementation of a Performance Test System for Missile Coordinator
    Zhang, Haifen
    Wu, Falin
    An, Guangqi
    Li, Min
    Zhao, Yan
    2015 INTERNATIONAL CONFERENCE ON INFORMATION SCIENCE AND INTELLIGENT CONTROL (ISIC 2015), 2015, : 253 - 257
  • [50] Analysis and design of missile guidance system with radome effects
    Qi, Baohua
    Zhang, Lin
    Kongzhi Lilun Yu Yinyong/Control Theory and Applications, 2000, 17 (04): : 500 - 504
12345