智能制造系统中的合作与协调

通过对智能制造系统结构和运行方式的介绍，分析了智能制造系统中合作与协调的特点，描述了基于改进合同网的谈判方式的制造任务分配方法，并提出分布式智能制造系统中各自治单元之间利用ＣＯＲＢＡ和分布式对象技术建立合作与协调基本环境的方法。     

空间交会对接的智能控制

本文探讨了交会对接过程自动寻的阶段的智能控制策略及绕飞和最后逼近阶段的模糊控制问题,并针对实际条件给出了仿真结果,证明本文介绍的控制策略是可行的。     

应用于智能化网络的LONWORKS技术

论述了应用于智能化网络的ＬＯＮＷＯＲＫＳ技术，介绍了ＬＯＮＷＯＲＫＳ技术的技术特点及采用ＬＯＮＷＯＲＫＳ技术系统的特点。对ＬＯＮＷＯＲＫＳ技术中的Ｌｏｎｔａｌｋ协议及其寻址方式、冲突检测算法和神经元（Ｎｅｕｒｏｎ）芯片的技术特点作了简单的介绍。     

专家系统在材料领域中的研究现状与展望

简要介绍了专家系统的一般结构及功能，综述了近年来专家系统在材料领域中的应用，即在材料优化设计、材料智能加工与智能控制、材料缺陷诊断与质量控制等方面国内外研究现状与取得的成果，探讨了今后的发展方向。     

基于加速度测量的柔性智能桁架结构振动主动控制实验研究

本文在只能获得加速度时，通过改变Leunberger观测器的结构形式，基于模态滤波器技术、最优控制理论和计算机控制系统理论，采用独立模态空间控制策略进行了具有密集模态的空间柔性智能桁架的实时计算机振动主动控制实验研究。实验结果表明这种控制策略是行之有效的。     

空间遥操作机器人系统控制参考模型

从分析智能系统中智能行为机制人手，研究了智能系统中自组织单元基本结构，基于智能工程中的集成单元结构，提出了遥操作机器人系统的递阶嵌套控制参考模型，并应用到遥操作空间机器人模拟实验中，完成了模拟舱内作业任务，验证了其实用性。     

旋转梁的动力学建模及其反馈控制

利用哈密尔顿原理,推导了刚柔耦合形式的旋转欧位－伯努利梁的动力学方程,并在小转速的假设下,给出了线性化近似方程的解析解;讨论了由直流电机和压电陶瓷组成的控制系统,并从动力学稳定的角度出发,利用Lyapunov第一方法设计系统的反馈控制实现了动力学稳定性。最后通过计算机仿真证明控制策略的有效性。     

航天器自主运行技术的进展

阐述了航天器自主运行的概念、目标和任务。对自主运行和传统测控方式进行了比较。最后重点介绍了航天器自主运行技术的进展情况。文章分4个部分介绍自主运行技术。首先介绍了2种自主运行体系结构，它们是自主运行各种功能集成的基础。第2部分介绍了2种智能规划与调度技术。第3部分介绍了基于模型的故障诊断与系统重构技术。第4部分介绍了有效载荷数据自主处理的进展情况。最后进行了总结并介绍了与自主运行相关的其他技术。     

Intelligent spacecraft module

The paper presents the development of an on-going research project that focuses on a human-centered design approach to habitable spacecraft modules. It focuses on the technical requirements and proposes approaches on how to achieve a spatial arrangement of the interior that addresses sufficiently the functional, physiological and psychosocial needs of the people living and working in such confined spaces that entail long-term environmental threats to human health and performance. Since the research perspective examines the issue from a qualitative point of view, it is based on establishing specific relationships between the built environment and its users, targeting people?s bodily and psychological comfort as a measure toward a successful mission. This research has two basic branches, one examining the context of the system?s operation and behavior and the other in the direction of identifying, experimenting and formulating the environment that successfully performs according to the desired context. The latter aspect is researched upon the construction of a scaled-model on which we run series of tests to identify the materiality, the geometry and the electronic infrastructure required. Guided by the principles of sensponsive architecture, the ISM research project explores the application of the necessary spatial arrangement and behavior for a user-centered, functional interior where the appropriate intelligent systems are based upon the existing mechanical and chemical support ones featured on space today, and especially on the ISS. The problem is set according to the characteristics presented at the Mars500 project, regarding the living quarters of six crew-members, along with their hygiene, leisure and eating areas. Transformable design techniques introduce spatial economy, adjustable zoning and increased efficiency within the interior, securing at the same time precise spatial orientation and character at any given time. The sensponsive configuration is programmed to exhibit behavior in direct relation to human activity. It is based upon two active systems, the Activity Evaluation System (AES) and the Response System (RS), with combined action that is always open to the control of the user. The AES monitors the daily schedule of the astronauts in order to find patterns of activity, understand the context of actions and moreover to assess the psychological condition of the crew-members. If it finds cause for intervention, AES will give way to the RS which employs smart materials, controllers and actuators in order to perform required changes in the environmental factors, both spatial (volume and surface) and ambient (audio, visual, olfactory, and haptic), and induce a desirable spatial and/or psychological condition that is beneficial for the astronauts? comfort and well being.     

挠性卫星高精度智能控制及物理仿真实验研究

从工程角度出发,以具有挠性太阳翼的卫星为背景,着重研究了挠性卫星的智能控制方案。针对高精度控制这一要求,设计了双层小脑模型神经网络(CMAC)与变结构(VSC)复合智能控制器,并基于单轴气浮台全物理仿真系统进行了实验,取得了较高的姿态控制精度,表明了智能控制方法的有效性。