姿态信息的英文

• attitude information
• attitudeinformation

• "姿态"英文翻译    gesture; posture; one's bear ...
• "信息"英文翻译    information; message; news
• "姿态信号" 英文翻译 :    attitude signal
• "俯仰姿态信号" 英文翻译 :    pitch attitude signal
• "滚转姿态信号" 英文翻译 :    roll attitude signal
• "偏航姿态信号" 英文翻译 :    yaw attitude signal
• "动态信息" 英文翻译 :    dynamic information; trends
• "控制态信息" 英文翻译 :    control state information
• "双态信息" 英文翻译 :    binary state information
• "状态信息" 英文翻译 :    information, status; state information; status information; status messages
• "状态信息帧" 英文翻译 :    sif status information frame; status information frame
• "组态信息" 英文翻译 :    configuration info
• "不定状态信息" 英文翻译 :    faulty state information
• "部件状态信息" 英文翻译 :    unit status information
• "电路状态信息" 英文翻译 :    circuit state message
• "动态信息结构" 英文翻译 :    dynamic information structure
• "动态信息转储" 英文翻译 :    dynamic dump
• "呼叫状态信息" 英文翻译 :    call status information
• "交易状态信息" 英文翻译 :    tsi，transaction status information
• "生态信息系统" 英文翻译 :    ecosystematic information system
• "室内状态信息" 英文翻译 :    room status information
• "通道状态信息" 英文翻译 :    channel status information
• "同步状态信息" 英文翻译 :    ssm synchronization status message; ssm:synchronous status message
• "系统状态信息" 英文翻译 :    system status information
• "信道状态信息" 英文翻译 :    csi channel state information

• ( 3 ) for a symmetrical distribution scene , the attitude information of the terrains is included in the variable of the orientation angle of the polarization ellipticity
  Cd对于一个均匀分仆场景，地势的姿态信息调制在极化椭圆力下0角的变化量中。
• A sampling process is designed to implement the computation of the observation likelihood , in which a proposed relation model between head and face of their position and size is used so as to achieve improved accuracy and efficiency in the fusion
  其中，利用检测器提供的姿态信息对头部和人脸的位置大小关系提出了一种模型，提高了观测模型融合的准确性和高效性。
• Aimed at the vermiculation characteristcs of the move - in - mud robot , its location system performs the orientation of the move - in - mud robot by means of relative oriention , using the attitude information and displacement information
  其定位系统针对拱泥机器人以蠕动方式运动的特点，利用机器人的姿态信息和拱泥头位移信息，采用相对定位的方法实现拱泥机器人的定位。
• The wandering explorer such as lunar rover in order to improve its existent ability and complete lunar exploration mission successfully , they have to carry out independent operation and management . among them , one of the key techniques is how to obtain the position and attitude of lunar rover
  月球车等漫游类探测器要提高生存能力并且成功完成科学探测任务,就必须实现自主运行和管理,其中关键技术之一是获取自身的位置和姿态信息。
• In modem war , a precise orientation and emendation system applied to artillery spying is needed , existing orientation and emendation system usually computes position of object according uav ( unmanned air vehicle ) ' s position and pose and the pose of vidicon on uav , but orientation is n ' t enough precise
  现代战争中需要高精度的炮兵侦察定位校射系统，然而现有的定位校射系统通常是根据无人机的位置、姿态信息和机载摄像机的姿态信息来估计目标区域的位置，定位精度不高。
• After analyzing the existing ambiguity resolution methods the dissertation investigates the baseline rotation method based on the antenna - swap idea , and develops the fixed axis rotation maximum - minimum method ? farmm and the equivalent rotation maximum - minimum method ? ermm applicable for static basement and moving vehicle respectively . the former lowers the demands on rotation device while the latter improves the flexibility of antennae installation . meanwhile the dissertation also brings forward an ambiguity function search method which needs only one single epoch data with the outer aided information , and investigates the accuracy requirements for the assistant pointing information
  其次,通过与gps等多星系统定向关键技术的对比分析,指出双星定向模糊度确定的难度;在分析现有模糊度求解方法的基础之上,研究了基于交换天线思想的转动基线模糊度确定方法,并提出了适合于静基座的定轴转动极大/极小值farmm法,以及适合于地面运动载体的等效转动极大/极小值ermm法,前者降低了对转动机构的要求,后者则提高了天线安装的灵活性;同时,提出了一种借助外部辅助信息的模糊度函数搜索法实现单历元双星定向,并分析了对外部辅助单轴姿态信息的精度要求。
• Based on extended kalman filter ( ekf ) algorithm , an traditional attitude determination scheme using star sensors and gyros was studied , and proved not able to achieve the required precision . so a new idea called instrument - in - loop was presented what using the attitude information contained in the payload ' s data for the control loop . the simulation proved that the instrument - in - loop method can greatly improve the precision of attitude determination with low cost
  建立了svom卫星各种姿态敏感器的测量模型，研究了基于推广卡尔曼滤波算法的“星敏感器+光纤陀螺”定姿方案，指出了其无法满足svom卫星的定姿精度要求，并提出了instrument - in - loop的思想，即利用卫星有效载荷测量数据中蕴含的高精度姿态信息来滤波定姿，从而在避免使用昂贵的星敏感器的同时大大提高了系统的定姿精度。
• The simulation results show that the feature point detection and tracking algorithm is feasible . next , matched points based essential matrix estimation is studied . the spacecraft attitude and position parameters are derived from essential matrix and the scale of motion is recovered with range information from laser ranger taken in account
  再次,研究基于匹配特征点对的本质矩阵的估计算法,给出了由本质矩阵求取空间探测器的姿态信息和位置信息的方法,并且结合激光测距仪信息,得到探测器的运动比例参数,实现软着陆过程的导航。