1.
spacecraft structural desig
太空飞行器结构设计
2.
In flight vehicle preliminary design it is necessary to quickly and economically estimate the aerodynamics of a wide variety of flight vehicle configuration designs.
在飞行器的初步设计中,快速而有经济地估计出飞行器结构设计中的各种气动特性是非常必要的。
3.
Research on MIMU System Design of Small Aircraft
微小型飞行器的MIMU系统结构设计方法
4.
Reliability Analysis and Optimization Design of Aircraft Structure;
飞行器结构可靠性分析与优化设计研究
5.
Research and Implementation on Architecture and Data Model for Aircraft Cooperative Design System;
飞行器协同设计系统体系结构与信息模型研究
6.
Design Optimization on Electromagnetic Scatter Property of Low Observable Aircraft Wing Structure;
飞行器翼面隐身结构电磁散射特性设计优化
7.
Design of Variable Structure Control System for Hypersonic BTT Vehicle
高超音速BTT巡航飞行器变结构控制系统设计
8.
Design for aerocraft attitude control system based on feedback-linearization and variable-structure-control
基于反馈线性化和变结构控制的飞行器姿态控制系统设计
9.
Research and Application of Product Structure and Configuration Management for Aircraft Cooperative Design;
飞行器协同设计中的产品结构与配置管理研究与应用
10.
Research on Product Structure and Configuration Management and the Application in Aircraft Cooperative Design;
产品结构与配置管理研究及其在飞行器协同设计中的应用
11.
Optimal Design Techniques Study with the Elastic Tailoring Application of the Aircraft Composite Structure;
飞行器复合材料结构弹性刚度剪裁优化设计技术研究
12.
Optimum Design of Optics Structure for Femto-Second Laser Based on Cr~(4+):YAG Crystal
Cr~(4+):YAG飞秒脉冲激光器光路结构的优化设计
13.
Design of Flapping Mechanism for a Micro Air Vehicle Based on Mathematical Morphology;
基于数学形态学的微扑翼飞行器翅翼机构设计
14.
Dynamics Simulation and Optimization Design of Driving Mechanisms of FMAV;
微扑翼飞行器动力学仿真及驱动机构优化设计
15.
Attitude Controller Reconfiguration for Spacecrafts with Abrupt Change of Centroid
一类质心突变飞行器的姿态控制律重构设计
16.
Design of three dimensional afterbody/nozzle configuration of airbreathing hypersonic vehicle
高超声速飞行器后体喷管三维构型设计
17.
Exploring Nonlinear Flight Control of Highly Maneuvering Fighter Aircraft
非线性结构自适应模型逆飞行控制律设计研究
18.
The tank location for these vehicles is chosen for optimum airframe design for axial loads.
这些飞行器上的油箱位置是相对轴向载荷作最佳结构设计来选择的。