卫星姿态控制系统的英文

• satellite attitude control system

• "卫星"英文翻译    satellite bit; particle
• "姿态"英文翻译    gesture; posture; one's bear ...
• "控制系统"英文翻译    navar; control system; opera ...
• "卫星姿态控制模拟器" 英文翻译 :    satellite attitude control simulator
• "姿态控制系统" 英文翻译 :    attitude control system
• "磁力姿态控制系统" 英文翻译 :    magnetic attitude control system
• "磁姿态控制系统" 英文翻译 :    magnetic attitude control system
• "单轴姿态控制系统" 英文翻译 :    single-axis attitude control system
• "地磁姿态控制系统" 英文翻译 :    magnetic attitude control system
• "机载姿态控制系统" 英文翻译 :    onboard attitude control system
• "冷气姿态控制系统" 英文翻译 :    cold gas attitude control system
• "数位姿态控制系统" 英文翻译 :    dacs digital attitude control system
• "主动姿态控制系统" 英文翻译 :    aacs active attitude control system
• "低温液体姿态控制系统" 英文翻译 :    cryogenic attitude control system
• "轨道飞行姿态控制系统" 英文翻译 :    orbital attitude control system
• "质量移动法姿态控制系统" 英文翻译 :    mass-motion attitude control system
• "质量移动姿态控制系统" 英文翻译 :    mass-motion attitude control system; mass-shifting; mass-motionattitudecontrolsystem; mass-shifting attitude control system; mass-shiftingattitudecontrolsystem
• "主动式姿态控制系统" 英文翻译 :    active attitude control system
• "姿态控制系统氮气瓶" 英文翻译 :    attitude control nitrogen gas bottle
• "卫星姿态" 英文翻译 :    attitude of satellite; satellite attitude
• "动态控制系统" 英文翻译 :    dynamic control system; kinetic control system
• "因态控制系统" 英文翻译 :    solid state control system
• "卫星姿态稳定" 英文翻译 :    satellite attitude stabilization
• "车身动态控制系统" 英文翻译 :    dcs
• "结构模态控制系统" 英文翻译 :    structural-mode control system

• The proposed controller is then designed and simulated with the attitude control of a spacecraft as an example
  文中以某小卫星姿态控制系统为例，对所提出的自适应控制器进行设计和仿真。
• Satellite attitude determination system is the important part of the attitude control system ( acs ) , and its accuracy is the key factor for the performance of the acs
  卫星姿态确定系统是卫星姿态控制系统中的重要组成部分,其精度是影响姿态控制系统精度水平的决定性因素。
• On the base of active disturbance rejection control , author use active disturbance rejection control in small satellite attitude control system and designs a two - loop active disturbance rejection attitude control system
  在深入研究了自抗扰控制理论的基础上,将自抗扰控制新技术应用于主动磁控小卫星姿态控制系统中。
• Space technology is the most influencing technology of moden science and technology . with widespread use of application satellite , people pay more and more attention to high accuracy and durability attitude control system
  航天技术是现代科学技术中最具有影响力的高技术之一,随着通信、遥感等卫星的广泛应用,高精度、长寿命的卫星姿态控制系统成为人们对卫星关注和研究的焦点。
• In order to study small satellite attitude control system , the author first establishes the small satellite dynamics , kinematic models , and gives the theories of the quarternion , then study in - depth of the principles of the active magnetic control
  为研究主动磁控小卫星姿态控制系统,首先建立了主动磁控小卫星动力学、运动学模型,并给出了姿态四元数的相关理论。从地磁场模型出发,深入研究了主动磁控的原理。
• The aim of this article is to shorten the gesture capture time and to improve control precision . author from both theoretical and applied researches the using of a nonlinear active disturbance rejection control technologies in small satellite gesture capture system
  本文以缩短主动磁控小卫星姿态捕获时间,提高控制精度为目标,从理论和应用两个方面深入研究了非线性自抗扰控制新技术及其在主动磁控小卫星姿态控制系统中的应用。
• This paper studies on the attitude ontrol system of three - axis stabilized satellite systematically , and makes deep study on the design of attitude control system . the main work of this paper is as follows : first , found whole mathematical model about attitude control system of satellite . it contains kinematics model , dynamic model , actuator model and torque model . analyse the conmmen characteristic of actuator of satellite ’ s attitude control system
  本文较为系统地研究了三轴稳定卫星的姿态控制系统,并在姿态控制规律的设计方面进行了较为深入的研究。论文主要工作如下:首先,建立了完整的卫星姿态控制系统的数学模型。其中包括星体运动学模型、星体动力学模型、执行机构模型及环境干扰力矩模型。
• Its results of application turn out to be satisfactory , especially in eliminating the outlier . in order to analyze and verify the telemetering data of the attitude control system , this dissertation uses mathematic simulation to acquire the standard data . the t - verification and correlation coefficient method are used to analyze the data consistency for analyzing the operating quality
  为定量地分析和检验卫星姿态控制系统的遥测数据,本文采用数学仿真的办法模拟实际飞行过程,得出相对标准的数据;采用t检验、相关系数法等办法对其与遥测数据做一致性检验,以分析遥测数据的合理性及系统的工作性能。
• The air bearing is the most important part of an attitude control system simulator for simulating a satellite moving in the weightless circumstance . performance of a satellite attitude simulation system based on air bearing is decided by the inertia matrix and gravity disturbance torque arising from a difference between mass center and rotation center , and air bearing can be used to simulate the algorithm of on - line mass - property parameters identification on the ground . so the problem of mass - property and gravity disturbance torque identification for satellite and air bearing is studied in this thesis
  气浮台能够模拟卫星在轨失重条件下的姿态运动,是卫星姿态控制系统物理仿真的核心部件,其转动惯量和质心偏移引起的重力干扰力矩等决定了基于气浮台的卫星姿态物理仿真系统的性能,并且利用气浮台可以实现卫星质量特性在线辨识算法的地面物理仿真验证,因此本文对卫星和气浮台的质量特性及干扰力矩在线辨识问题进行深入研究。
• Based on the spaceflight technology innovation program of “ research on the testing method of reliability - - - - research on the fault diagnostic expert system and neural network ” and the pre - research defense projects of “ research on longevous service and high reliability of satellites ” of the national tenth - five - year plan , taking attitude control system of a satellite as object , the theories and the applications of the neural networks and expert system in the fault diagnosis are studied in this dissertation
  本文以航天技术创新基金项目“可靠性试验方法研究? ?故障诊断的专家系统神经网络技术研究”和国家武器装备“十五”预研项目“卫星长寿命高可靠性技术”为背景,以卫星姿态控制系统为研究对象,在理论和实践两个方面对神经网络和专家系统相结合的故障诊断技术及其在卫星中的应用进行了研究。