指向控制的英文

• pointing control

• "指向"英文翻译    directing; sensing; sense of ...
• "控制"英文翻译    control; dominate; regulate; ...
• "天线指向控制" 英文翻译 :    antenna direction control
• "太阳帆板指向控制" 英文翻译 :    solar array pointing control
• "侧向控制" 英文翻译 :    lateral guidance
• "垂向控制" 英文翻译 :    vertical control
• "单向控制" 英文翻译 :    unidirectional control
• "单向控制板" 英文翻译 :    one-way board
• "导向控制" 英文翻译 :    lead control
• "导向控制管" 英文翻译 :    pilot line
• "定向控制" 英文翻译 :    directional control; orientation control
• "反向控制" 英文翻译 :    reverse control
• "反向控制器" 英文翻译 :    reversing controller
• "方向控制" 英文翻译 :    direction control; directional control
• "方向控制阀" 英文翻译 :    directing-control valve; directioal control valve; direction control valve; direction-control valve; directional control valves; directional controls
• "方向控制器" 英文翻译 :    direction controller
• "航向控制" 英文翻译 :    yaw controlcourse control
• "横向控制" 英文翻译 :    lateral control; transverse control; traversal control; traverse control
• "换向控制" 英文翻译 :    reverse control
• "换向控制杆" 英文翻译 :    reversing control lever
• "换向控制架" 英文翻译 :    reversing gear control bracket; reversinggearcontrolbracket
• "换向控制器" 英文翻译 :    reversing controller
• "逆向控制" 英文翻译 :    reversing control
• "双向控制" 英文翻译 :    bilateral control; two way control; two-way control
• "双向控制器" 英文翻译 :    reversed controller; reversible controller

• This control method effectively solves the problems of the antenna tracking - pointing control
  该控制方法有效地解决了天线跟踪指向控制问题。
• The simulation and validation are conducted for the antenna pointing control system designed before
  最后对设计的天线指向控制系统进行了仿真验证。
• Aiming at satellite - satellite pointing / tracking system , an experiment based on xpc real - time simulation platform is designed
  针对星星天线指向控制系统,设计了以xpc为实时仿真平台的数据实验。
• The satellite attitude control system is modeled into a close control loop with three momentum wheels on each axis
  星体姿态控制系统采用三轴稳定动量轮闭环控制模型，天线指向控制系统采用开环控制。
• Next , the characteristics of the user satellites complex control system is that the high accuracy antenna pointing control is realized on the basis of ensuring the high accuracy attitude stabilization control of the satellite body
  3 .用户星复合控制系统的特点是在保证卫星平台高精度姿态稳定控制的前提下,实现星间链路天线的高精度指向控制。
• Then , the tracking laws for the user satellites antenna pointing to the tdrs which is fit to the engineering application are derived , and the basic concepts of the user satellites antenna pointing control project are described in detail
  2 .推导出了适合于工程应用的星间链路天线跟踪中继卫星的跟踪规律,详细的论述了星间链路天线指向控制策略。
• The antenna pointing control accuracy can satisfy the design specification and it is validated to be appropriate and effective . at last , the designed user satellites complex control system is simulated based on xpc target which is used for hardware - in - the - loop simulation
  4 .基于xpc实时仿真平台,充分利用实验室条件,搭建了用户星天线样机在回路中的半物理仿真实验,将天线指向控制系统和星体姿态稳定控制系统联合起来,组成中继卫星复合控制系统进行近一步的验证。
• Based on chinese tracking and data relay satellite ( ctdrs ) in the future , the antenna pointing control and complex control theory of user satellite are studied deeply in this dissertation , which is funded by the improve item of dept . of astronautic engineering and mechanics ? “ the teaching demonstration of antenna pointing control system in tdrss ” . the main contents of this dissertation are consisted of the following parts : firstly , dynamics equation is derived using lagrange equation for user satellite , so as the kinetics equations of user satellite at the same time are expressed in the form with matrix differential equations that is suitable for attitude control system design and analysis
  本学位论文结合航空宇航科学与技术学科研究生教学基地实验室建设项目“中继系统星间链路天线指向控制系统教学与演示实验” ,以我国跟踪与数据中继卫星系统为背景,对某型号用户星星间链路天线指向跟踪控制和复合控制理论进行深入的研究,研究内容主要包括以下几个方面: 1 .利用lagrange方程建立了用户星的动力学方程,同时推导了运动学方程,并将这组动力学方程以矩阵微分方程形式表示,使之适用于姿态控制系统的设计和分析。
• The satss is an antenna pointing servo system with ultra - low speed and high accuracy , driven by a rare earth permanent magnet ( repm ) brushless dc torque motor . to reduce torque ripple , the repm brushless dc torque motor has a slotless armature , and uses sinusoidal wave driven technology
  卫星天线跟踪伺服系统为超低速高精度天线指向控制系统，该系统使用稀土永磁式无刷直流力矩电机作为天线的驱动机构，为降低转矩脉动，电机采用无槽电枢结构设计，并使用正弦波驱动方式。
• To simultaneously solve the problems of the robustness , decoupling control and high accuracy tracking control at the high tracking rate in antenna control system , a new nonlinear antenna tracking - pointing control system for user - satellite was proposed based on a unique nonlinear active disturbance rejection control method
  摘要为同时解决用户卫星天线控制系统的鲁棒性、解耦控制和高跟踪速率下的高精度跟踪控制等问题，采用非线性自抗扰控制方法，提出了一种新型的用户卫星天线跟踪指向控制系统。