1.
Integrated Design of Integral Rocket-Ramjet Missile;
整体式冲压发动机导弹总体一体化设计
2.
An Optimization Framework for Missile General Design with Multi-method Collaboration Support;
支持多方法协作的导弹总体设计优化框架研究
3.
Research on the Optimization System of Missile Integration Design Based on RSM;
基于RSM的导弹总体设计优化系统研究与实现
4.
Evaluation Method of General Schemes of Missile: Theory and System Implementation;
飞航导弹总体方案评价方法研究及系统实现
5.
Study on the Scheme for Long-Range Air-Defense Missile With Multidisciplinary Design Optimization;
运用MDO进行远程防空导弹总体方案研究
6.
Processing Methods of Coupled Relationship of Multidisciplinary Design Optimization for Missile
导弹总体多学科设计优化耦合关系处理方法
7.
Research on Process Model Based Framework of General Missile Design Optimization and Its Key Technologies;
基于过程模型的导弹总体优化设计框架及其关键技术研究
8.
The idea and method in this paper can be taken as a reference for the design of terminal homing anti-tank missiles and accuracy allocation of weapon system.
文中结果可为末段寻的制导的反坦克导弹总体设计及武器系统精度分配提供参考。
9.
Study on Smart Morphing Missile Aerodynamic Configuration Conceptual Design;
智能可变外形导弹的气动外形总体设计研究
10.
hard missile base
混凝土掩体导弹基地
11.
SPIRBM (Solid Propellant Intermediate Range Ballistic Missile)
固体推进剂中程弹道导弹
12.
The Conflict of Attack and Defence System Between TBM and ATBM
地地弹道导弹武器系统攻防体系对抗
13.
Adaptive Parameter Estimation for Transverse Vibration of the Flexible Missile
弹性体导弹横向振动自适应参数估计
14.
Influence of Position Change of Projectile Pressure Center on Trajectory of Terminal Guidance Shell
弹体压心位置变化对末制导炮弹弹道的影响
15.
Design of Missile Dynamic Measurement System Based on VXI Bus
基于VXI总线的导弹动态测试系统设计
16.
Design of Missile Launch Control System Based on FlexRay Bus
基于FlexRay总线的导弹发射控制系统设计
17.
Design of Control Node of Missile Based on FlexRay Bus
基于FlexRay总线的导弹控制节点设计
18.
The TMD system is a rehashed version of former U.S. president Reagan's star wars defense shield
战区导弹防御体系是美国前总统里根执政期间星球大战防御体系的翻版