Development on camera monitoring system used in the large manned spacecraft environment simulation lab

The foundation of integrated prediction system of spacecraft environment and research of virtual integrated assembly techniques, the space-ground integrated application system of space environment and the production system of integrating assembly and space environment test are the future trend and the development modes of spacecraft environment engineering.

航天器环境效应综合预示系统及航天器虚拟总装工艺技术，是未来发展的趋势；而建立空间环境天地一体化应用系统和建立空间环境试验与总装生产体系，是未来发展的模式。

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It is pointed out that the environment test evaluation and protection technology of spacecraft for high reliability and long life will be the emphasis of the development and research work in the field of spacecraft environment engineering in long term.

文章指出：开展高可靠、长寿命航天器环境试验评价及防护技术研究，是航天器环境工程的长期重点发展方向；

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Cost Models, Revenue Models, Examples from Aircraft, Spacecraft and Automotive Engineering.

成本模型，收益模型，来自飞机、航天飞机和汽车工程的例子。

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The paper discusses the importance of spacecraft environment engineering in the verification work of space products. Brief description is given concerning the practice in foreign countries and related standards. A brief introduction of space product verification standard MIL-STD-1540D is also given in the paper.

论述了航天器环境工程对航天产品验证工作的重要性，介绍了国外的实践与有关标准，着重介绍了美军标MIL-STD-1540D中对航天产品的验证要求。

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Taking attitude motion of spacecraft as engineering background for exploring chaos, and 3-axis air bearing table as experimental equipment, a series of investigation on control and anti-control for chaos was carried on.

以航天器姿态运动为工程背景，以三轴气浮台为物理实验平台，研究了混沌控制与反控制问题；

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Furthermore, this work would be extended to apply in the configuration and layout design of other spacecraft, engineering machinery, tunnel boring machine ( TBM), shipping, bullet train, etc..

本文的研究具有理论意义和应用价值，可望推广应用于其它航空航天器、工程机械、隧道掘进机、船舶、高速列车等领域的配置和布局一体化设计。

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In the new century, the spacecraft environment engineering will continuously pay great attention to improve the test efficiency and at the same time to reduce test costs and time.

在新的世纪，环境工程的发展在继续努力降低环境试验的费用和时间的同时，提高环境试验的效果，使整个环境工程对保证航天器可靠性起到更重要的作用。

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The study of methods for reducing or avoiding its effects, that is" spacecraft immunity engineering for environment", has also been done.

对为了避免和减少环境效应影响的工程方法进行了探究。

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The applied software system of the spacecraft T.T.C Engineering

航天测控工程的应用软件系统

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Spacecraft environment engineering ( 2002) contents

《航天器环境工程》（2002）总目次

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The spacecraft environment engineering in 21 century

21世纪的航天器环境工程

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Dynamic membrane and its application in environment engineering SPACECRAFT ENVIRONMENT ENGINEERING ( 2001) CONTENTS

动态膜技术及其在环境工程中的应用《航天器环境工程》（2001）总目次

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Using power flow theory, the vibration damping characteristics of typical interconnected structures in spacecraft engineering are studied in this paper.

本文利用功率流理论对航天工程中典型减振连接结构的减振特性进行了研究。

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Dynamic Modelling of Liquid-Solid Coupling System with Container in Spacecraft Engineering and Investigating of its Coupling Mechanism

航天工程中的贮箱类液固耦合动力学建模及耦合机理研究

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Quantitative analysis of human performance in microgravity is important for both scientific investigations and spacecraft engineering design.

定量的分析人类在微重力环境下的活动，对科学研究和太空船工程设计均很重要。

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The method in this paper may find applications in the Spacecraft Engineering and machine system designs.

文中方法可应用于航天器、机构等动力学方程推导。

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Vibration control technologies have wide applications in the field of spacecraft engineering.

在航天工程领域，减振技术得到了越来越广泛的应用。

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A new method is promoted for flexible spacecraft control by describing flexible spacecraft dynamics equations as T-S fuzzy model and designing a PDC fuzzy controller.

将挠性航天器姿态动力学方程描述为T-S模糊模型为挠性航天器控制提供了新思路；

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The simulation results demonstrate the feasibility and effectiveness of the proposed method. A robust active control approach is presented for the attitude tracking control and vibration damping of a spacecraft with actor dynamics.

针对带有执行机构动态特性的挠性航天器姿态跟踪问题，基于后步滑模及主动振动控制技术提出一种鲁棒主动控制策略。

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In order to verify the dynamics characteristic of a space remote sensing camera, spacecraft and camera dynamics coupling test is needed.

为了检验空间遥感相机的动力学特性，需要对相机与飞船进行动力学耦合试验。

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