航天器设计

基于计算机的低地球轨道航天器设计与观测的轨道碎片环境模型

A computer-based orbital debris environment model for spacecraft design and observations in low-Earth orbit

航天器设计常用算法及其应用

Spacecraft Design Common Algorithms with Applications

本文简要概述了动力学在航天器设计领域的部分应用情况，着重体现了CAE仿真在工程设计中的应用进展。

In the paper , some successful application of dynamics in the design area of spacecraft are presented and the advance of CAE simulation technique in practical engineering is emphatically discussed .

热屈曲是航天器设计中经常遇到的问题，对于含开口薄壁杆件的大型空间柔性结构来说，热屈曲问题尤为严重。

Thermal buckling is a common problem for space structure design .

航天器设计与制造中的知识产权工作

Work on IPR in Design and Manufacture of the Spacecraft

节约重量是航天器设计的普遍原则之一。

As is well known that the saving the weight is one of the universal principles of spacecraft design .

在充液航天器设计中有时需要考虑微重力环境下的液体晃动。

Liquid sloshing under low gravity environment is a problem that must be considered during general design of liquid-filled spacecraft .

空间碎片减缓设计是实现空间碎片减缓的主要措施，已成为航天器设计的重要组成部分。

Space Debris Mitigation is one of important parts of designing spacecrafts and plays the main role of mitigating Space Debris .

现代的航天器设计中愈来愈重视利用计算机技术，计算机算法的研究与应用也愈来愈引起人们的关注。

Computer technology is regarded more and more in modern spacecraft design , thus people pay more attentions to the study and application of the computer algorithms .

研究成果有助于丰富和发展孔洞型细观损伤理论，亦对航天器设计有所裨益。

The achievements of this work are helpful for developing and expanding the theory of meso-damage and also of great benefit to the design of space vehicles .

微流星体及空间碎片防护结构设计，是航天器设计的一个重要问题。

In order to ensure the astronauts safety and spacecraft normal operation , the design of meteoroids and space debris protection configuration become an important problem of spacecraft design .

将基于人体测量参数的数字人体模型应用于载人航天器设计方案的仿真评价对发现设计缺陷，提高整个系统的安全可靠性具有重要意义。

It is very important to find design defects and to improve the system reliability when digital human models based on anthropometric data are applied in simulation of manned spacecraft design scheme .

空间碎片减缓是要求限制和清除空间碎片，它贯穿于航天器设计、生产、发射、运行以及完成任务以后的全过程。

Space Debris Mitigation requires restraining and clearing the Space Debris , which is of great importance during the whole process of designing , manufacturing , launching , operating and completing tasks of spacecraft .

更加多样化航天器设计公司精心选择结果，这反映了不同的技术解决方案来面对地球之外的挑战，而且这也改变着未来。

More diverse are the spacecraft designs the companies have chosen , reflecting not only different technical solutions to the challenges of flying people beyond Earth , but also their alternative visions of the future .

航天器设计面临任务复杂度增加、设计周期缩短、研制经费受限等多重压力，传统的设计理念已不再适应经济发展和军事应用的需要。

Spacecraft designers are faced with such new challenges as more complex space missions , shorter design durations and more tightening budgets . The traditional design philosophy becomes insufficient for the needs of the economic development and military applications .

通过设计这些部件的设备模拟器，用其代替真实部件引入闭环回路，是一种工程上实用有效的方法，目前在国内外的航天器设计中已得到了广泛的应用。

Through the design of these parts of the device simulator , with its introduction of closed-loop instead of the real device is a practical and effective engineering method . Current the way has been widely used at home and abroad .

结构的振动现象随处可见，在航天工程中，结构振动更是一个尤为重要的问题，因而振动控制成为航天器设计的一个重要研究领域。

The structure vibration can be seen everywhere , especially in space engineering , it is a problem that need to be paid too much attention on , as a result , the vibration control is a very important field in aircraft designing .

一旦进入太空的成本下降，人们可以做的其他的事情就可以极大地增加。这是一种全新的航天器设计，飞船就好比飞机，乘客可以是冒险者或者太空爱好者，而不一定必须是专业的宇航员。

Once the cost of putting something into space goes down , the number of things you can afford to do goes up greatly . It 's a new ear of spacecraft design , in which spaceships can be treated more like aircraft and the passengers won 't be professional astronauts , but adventure seekers or space enthusiasts .

计算结果对以后MPT真空羽流场测试和航天器一体化设计提供了参考。

The results can provide reference for the testing of MPT vacuum plume and integral design of spacecraft .

介绍塑料挤出模制造业CIMS的研究背景和研究基础，结合塑料挤出模制造业的特点讨论塑料挤出模CIMS的关键技术、总体框架设计和数据流设计；航天器协同设计平台总体框架设计

The background and base of the research in CIMS on manufacturing of extrusion tooling for plastics profiles are introduced . The Overall Framework of the Digital Cooperative Design Platform for Spacecraft

航天器协同设计平台总体框架设计关于素质教育的思考

The Overall Framework of the Digital Cooperative Design Platform for Spacecraft

模糊可靠性理论在航天器舱段设计中的应用

Application of Fuzzy Reliability Theory for Design of Flying Vehicles

航天器轨道设计系统的小型化实现

Realization of A Small System of Spacecraft Orbit Design

数字人体在载人航天器方案设计模型仿真中的应用研究

Study on Application of Digital Human Model in Simulation of Manned Spacecraft Design Scheme

航天器轨道设计因卫星应用目的和总体设计方案的不同而灵活多样。

Orbit design of Spacecraft is agility due to different application and overall solution .

改善大型结构的动态特性对航天器总体设计具有十分重要的意义。

To improve the dynamic properties of cabin structure are of great significance for spacecraft .

本文给出了航天器协同设计平台总体框架的方案。

This paper gives a scheme for the overall framework of a spacecraft cooperative design platform .

正确的分析和预测整个系统的动力学行为是在航天器总体设计中必须解决的关键问题。

Analyzing and forecasting the dynamic behavior is very important for the overall design of the spacecraft .

该项工作对航天器的设计具有指导意义。

As a result , the present work provides a good guideline to the design of spacecraft .

撞击损伤特性研究是航天器防护设计的一个重要问题。

An investigation into the impact damage characteristics has become an important problem for spacecraft protection design .