姿态敏感性,pose sensitivity
1)pose sensitivity姿态敏感性
2)inertial attitude sensor惯性姿态敏感器
英文短句/例句
1.An Overview of Fault Diagnosis Methods for Inertial Sensing Device on Spacecraft星上惯性姿态敏感器故障诊断方法评述
2.Micro Attitude Determination System Based on MEMS Inertial Sensors基于MEMS惯性传感器的微型姿态测量系统(英文)
3.Application of iMEMS on Airplane Model Pose Testing System;微型惯性传感器应用于飞行器模型姿态测试的研究
4.Research on Information Fusion Method for Satellite Attitude Determination Based on Multi-Sensor Measurement多姿态敏感器测量的信息融合定姿方法研究
5.CMOS Star Sensor System Design;CMOS星敏感器卫星姿态定位系统设计
6.Federated SSUKF for Multi-sensor Spacecraft Attitude Estimation多敏感器联邦SSUKF融合姿态确定算法
7.Sensitive Mechanism of Micromachined Airflow Omnibearing Posture Sensor微机械气流式全方位姿态传感器的敏感机理
8.Analytic Solution for Attitude of Deep Space Explorer Based on Star Sensors基于星敏感器的深空探测器姿态解析算法
9.The Software Design of Star Sensor Pose-ascertaining System;基于星敏感器的姿态确定软件系统设计
10.Tradeoffs of Two Star-Tracker-Based Attitude Determination Algorithms基于星敏感器的两种姿态确定算法比较分析
11.Autonomous Navigation Based on Attitude Sensors for CBERS-02B基于资源一号02B卫星姿态敏感器的自主导航
12.MEMS Inertial Sensor-based Single Axis Strap-down Attitude Measuring Device基于微机械惯性器件的单轴捷联姿态测量装置
13.Assessing susceptibility of inertial measurement unit in flight craft to electromagnetic interference飞行器惯性测量组合的电磁敏感度评估
14.Filtering Algorithm for Satellite Attitude Determination and Sensor Alignment Calibration;卫星姿态确定及敏感器误差修正的滤波算法研究
15.Research and Implementation of Attitude Determination for FY-4 Meteorological Satellite Based on Star Tracker基于恒星敏感器的风云四号气象卫星姿态确定方法研究及实现
16.Attitude determination method of micro satellite under normal and failure mode of sensor敏感器正常和故障模式下微小卫星的姿态确定方法
17.Effect of environmental temperature on the sensitivity of the airflow level posture sensor环境温度对气流式水平姿态传感器灵敏度的影响
18.In practical applications, it is available to use multiple micro-inertial sensors to detect some outside infoumation.在实际应用中往往采用多微惯性敏感器来测定某些外界信息。
相关短句/例句
inertial attitude sensor惯性姿态敏感器
3)gesture sensitivity姿态敏感
4)Attitude sensor姿态敏感器
1.The fusion of multiple attitude sensors for ADS which consists of inertial measurement unit(IMU),horizon sensors and sun sensors,is performed via neural network architectures,back-propagation(BP) algorithm and Radial Basis Function(RBF) network are adopted separately,and the simulation is processed using the STK(Satellite Tool Kit) data in the present study.为得到高姿态精度,针对由惯性测量单元(Inertial Measurement Unit)、红外地平仪和太阳敏感器组成的卫星姿态确定系统,分别采用BP网络算法和径向基(RBF)网络算法对不同的姿态敏感器的输出数据进行融合,并用STK(Satellite Tool Kit)数据进行了仿真。
5)attitude quickness姿态敏捷性
1.According to those requirements,the dynamic response characteristics and the bandwidth were analyzed,along with the control characteristics and theattitude quickness.按照两种规范的要求,对纵列式直升机的动态响应特性与带宽、操纵特性与姿态敏捷性、轴间耦合以及横向突风扰动影响进行了分析,最后给出了一些有意义的结论。
6)optical-electronic attitude sensor光电姿态敏感器
延伸阅读
姿态①体态；姿势：姿态美丽。②态度：高姿态地让步。
