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空间飞行器
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  spacecraft
    Decoupling Sliding Mode Control in a Nonlinear Spacecraft System
    非线性空间飞行器系统的解耦滑模控制
短句来源
    In recent years, more and more attention has been paid on the theory and application research of Nonholonomic control systems which is involved in the study of constrained robot, spacecraft etc. .
    近年来非完整控制系统的理论与应用研究受到越来越广泛的关注,它的应用涉及到受限机器人、空间飞行器等许多领域,开展对它的研究在工业和国防等方面有着深刻的意义。
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    Tilt measuring is an expertise that can be used in making sure the incline of the spatial objects. This technology may be applied in many aspects, such as inertia measuring system of spacecraft, incline measuring of vehicle and hull,contrail detecting of broach.
    测斜技术是确定物体在空间的倾斜和倾向的专门技术,它应用于空间飞行器的惯性测量系统、车船体倾斜测量、工程钻孔轨迹检测等许多方面。
短句来源
    This method especially applies to the accurate thermal calculation for theouter parts of spacecraft.
    此方法尤其适用于空间飞行器外露部件的精确热计算。
短句来源
    A control method with sliding mode of nonlinear spacecraft system is provided in this paper, in which the interactive influences among channels of strong nonlinear spacecraft system are decoupled.
    提出了非线性空间飞行器系统采用滑动模态控制方法 ,它对强非线性的空间飞行器系统通道间交叉影响进行解耦 .
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    With the development of remote sensing technology,there's the general problem of huge data and the increasing demand of real-time image processing in the application of image compression.
    随着遥感技术发展,传输型空间飞行器系统中传输大量遥感数据的需求日益增加,对图像压缩处理能力提出了更高的要求,而现今相对落后的遥感图像压缩设备与海量数据压缩需求形成了矛盾。
短句来源
    This method especially applies to the accurate thermal calculation for the outer cavities ofspacecraft.
    此方法尤其适用于空间飞行器外露腔体的精确热计算。
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    Theoretical analysis and simulation results show that the proposed SMC law is globally stabilizing and insensitive to both parameter variations and external disturbances.
    理论分析及仿真结果表明 ,本文所求控制律对空间飞行器跟踪系统具有全局稳定性和鲁棒性。
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    A novel 4-DOF parallel robot that can fulfill gates docking in situation of rescue for aircraft or submarine is designed.
    笔者设计出一种可以在潜水艇和空间飞行器救援对接中实现对接的 4自由度的并联机器人机构。
短句来源
    This paper analyzes the superiorities and shortcomings of traditional trend-removal methods and puts forward a method based on wavelet transformation to remove the trend of non-stationary signals.
    分析了空间飞行器遥测信号处理传统趋势项剔除方法的优势和不足,提出了基于小波变换的非平稳信号趋势项剔除方法。
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  spacecraft
This collection can be used to test spacecraft production materials, in order to determine their resistance to biodegradation.
      
Studying Stability of the Flexible Spacecraft with a Discrete Control System
      
Stability of the spacecraft was considered with regard for its elastic structural oscillations arising under discrete control.
      
Consideration was given to the possibility of estimating jointly the motion coordinates and parameters of the elastic spacecraft using algorithms based on the discrete Kalman filtering and the theory of testing statistical hypotheses.
      
Design of the Suboptimal Profiled Relay Control of Orientation of the Spacecraft Having Elastic Structural Elements with Regard
      
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According to the probabitity theory,the geometric factors for Earth-thermal and Earth-reflection are calculated by random simulant method in this paper.The calculation process iseffectively simplied.This method especially applies to the accurate thermal calculation for theouter parts of spacecraft.

根据概率论的基本原理,用随机模拟法分别对轨道空间地球反照和红外辐射的角系数进行了计算,有效地简化了计算过程。此方法尤其适用于空间飞行器外露部件的精确热计算。

According to the probability theory, the radiation of the earth-reflection in complexcavity has been calculated by random simulant method in this paper. The distribution of thedirectional radiant intensity of the earth-reflection in orbits has been effectively simulated.This method especially applies to the accurate thermal calculation for the outer cavities ofspacecraft.

根据概率论的基本原理,用随机模拟法对空间光学遥感器外这光罩的地球反照辐射进行了计算,有效地模拟了任意空间位置的阳光反照的定向辐射强度分布。此方法尤其适用于空间飞行器外露腔体的精确热计算。

An approach to the calculation the view factors and orbit external thermal fluxes of the sun radiation, the earth radiation and its reflection on a space optical remote sense are described on the assumption of discrete plane, and the corresponding computer program and interface program with software PATRAN are developed. The software has found application in the thermal engineering analysis of a space optical window system. Moreover, basically, it is also suitable for other space projects.

简述了采用离散平面假设,计算空间光学遥感器的太阳辐射、地球红外辐射及地球阳光反照角系数和轨道外热流的方法。结合空间工程的结构、轨道参数和工况要求,设计开发了其实用计算软件以及与PATRAN软件进行数据传递的接口软件。该方法和软件已在实际工程的热分析计算中得到应用,适用于空间飞行器轨道外热流的计算。

 
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