Advances in the Spacecraft Autonomous Navigation Technology

Tracing Area Design for Spacecraft The optimization technology of block-wide injection profile control

空间飞行器追踪区设计区块整体调剖优化设计技术研究

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Analysis on Micro-vibration Environment of Spacecraft and Measurement Technology

航天器微振动环境分析与测量技术发展

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The paper briefly describes the application of spacecraft recovery technology in developing new space program, introduces some case of real application in developing strategic and tactical weapons and boosters, explains the effect and significance of spacecraft recovery technology in the process of space program developing.

文章简迷了飞行器回收技术在新型号研制中的应用情况，介绍了战略和战术武器及助推器具体的应用事例，说明飞行器回收技术在型号研制过程中的作用及意义。

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The application status of the spacecraft EPS technology researched and developed by Shanghai Academy of Spaceflight Technology ( SAST) during half century in the field of Chinese satellite, spaceship and international satellite was described.

阐述了近半个世纪以来，上海航天技术研究院在航天器电源研制技术方面所取得的成就及其在国内卫星、飞船和国外卫星领域的应用情况。

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Spacecraft simulation technology is a combined product of system simulation and aerospace engineering, which is a cornerstone of aerospace industry.

航天器仿真技术，是系统仿真与航天工程相结合的产物，是航天事业取得发展的基石。

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The Progress of Shanghai Spacecraft EPS Technology in the 20th Century

20世纪上海航天器电源技术的进展

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The development of spacecraft vacuum technology in China is expected.

展望了中国航天器真空技术的发展。

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But China has also achieved stunning progress with technology breakthroughs in such vital fields as wireless communications, permanent magnetic levitation rail transport, missile and spacecraft technology, and much more.

不过，中国也实现了惊人的进步，它在无线通信、磁悬浮运输、导弹和空间技术等很多重要领域都取得了技术突破。

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The special environment of a spacecraft with electric propulsion and its effects

电推进航天器的特殊环境及其影响

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A Hall thruster, with its high-efficiency and high specific impulse, is one of the most important electric propulsion devices widely used for spacecraft propulsion such as attitude control, orbital transfer and deep space exploration missions in the future.

霍尔推力器作为一种等离子体装置，以其高效率高比冲等特点成为国际电推进领域的研究热点，广泛应用在姿态控制，轨道转移及将来的深空探测任务。

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In particular, the Bond-graph-based method and the Miniature Mode Estimation system can used to detect and isolate faults in spacecraft propulsion system.

针对混合系统的故障检测与诊断问题，本文以推进系统为对象，研究了键图理论和Miniature Mode Estimation方法在其故障检测与隔离中应用与实现方案。

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Based on the physical and mathematical model of spacecraft propulsion system, the application of model based fault diagnosis method to the propulsion system of spacecraft was studied.

在飞船推进系统的物理和数学模型的基础上，研究了基于模型的故障诊断方法在飞船推进系统中的应用。

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By applying the diagnosis method proposed to the spacecraft propulsion systems, the results show that the relation-based fault diagnosis method is effective.

以空间推进系统为研究对象进行了实例诊断分析，结果表明：该方法是一种有效的基于定性模型故障诊断方法。

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Numerical simulation of liquefied gas self-pressurization for small spacecraft propulsion systems

小型航天器液化气推进系统的数值模拟

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Model-based fault diagnosis system for the spacecraft propulsion system

基于模型的航天器推进系统故障诊断

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Dynamic characteristics of priming process in spacecraft propulsion system(ⅰ) theoretical model and simulation results

航天器推进系统管路充填过程动态特性（1）理论模型与仿真结果

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Dynamic Characteristics Study of Spacecraft Propulsion System Engine

航天器推进系统发动机动态特性研究

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Numerical simulation on atomic oxygen action to spacecraft surface material& polyimide in Leo

低地球轨道环境原子氧对航天器表面材料聚酰亚胺作用的数值模拟

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Experimental investigations of the respective and synergistic effects of vacuum ultraviolet radiation and atomic oxygen on a spacecraft material& Kapton

空间材料Kapton的真空紫外与原子氧复合效应研究

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Wind-Induced Response Analysis of Spacecraft-Launching Tower

航天器发射塔风振响应分析

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