1) attitude errors
姿态角误差
1.
A new method is proposed to judge the observability of the attitude errors in integrated system, which utilize the variance matrix of the local observability matrix eigenvalue and eigenvector.
提出一种新的判断系统可观测性和可观测度的方法,详细分析了机体各种运动对系统姿态角误差可观测性和可观测度的影响,并把该方法应用于组合导航系统的可观测性和可观测度的研究中。
2.
It has been shown by the research results that, by means of implementing sine level maneuver flight, the local observability of the attitude errors can be increased, the flight alignment time can be reduced obviously, and the attitude errors can be cut.
从研究INS GPS(InertialNavigationSystem GlobalPositioningSystem)组合系统的姿态角误差可观测性出发 ,首次将局部可观测性理论应用于INS GPS组合系统 ,定量地计算出各种不同机动方式的局部可观测矩阵的条件数 ,找到了提高姿态角误差可观测性的最佳机动方式 。
2) attitude angle and course angle error
姿态、航向角误差
3) attitude error
姿态误差
1.
Analysis of the first crystal Attitude error in a double-crystal monochromator
双晶单色仪第一晶体初安装姿态误差分析
2.
This paper also derives some theortiacl formulas of the working reference plane attitude error through the error separating and compensating technology,which is proved by an experiment system.
首先建立了大型回转工作台的物理模型,根据这一模型建立了工作基面对地理坐标系的姿态变换矩阵,采用全微分法进行误差分离,推导得到了工作基面的姿态误差理论公式,并用一试验系统进行了验证。
3.
The dynamic equation of the relative attitude error between the missile and the ship has been built and the corresponding detection equation derived in the attitude transfer alignment based on the general error dynamic equation and velocity detection equation of INS.
在惯导系统一般的误差动态方程和速度观测方程的基础上,建立了姿态传递对准所必需的弹、舰相对姿态误差方程和观测方程。
4) constant angular error
姿态角常差
1.
In this paper a calibration model of constant angular error is introduced to enhance attitude precision by few ground control points (GCP).
简要叙述高分辨率卫星遥感影像的严格几何模型,建立影像姿态角常差检校模型。
5) position-stance error
位置和姿态误差
1.
From the six-freedom-degree parallel mechanism CMM position analysis, and using the matrix com-plete differential-coefficient theory, the relationship between original machine error and probe position-stance error is established.
为了探讨并联坐标测量机的机构原始误差和测量过程误差引起测量结果的偏差,在并联六坐标测量机的位置分析基础上,依据矩阵全微分理论,提出了机构原始误差与测头的位置和姿态误差模型,研究了机构参数误差变化对测头的位置和姿态误差的影响,明确了减小测头误差的主要途径是提高测量机零部件的机械加工和装配精确度,严格控制角度误差。
6) antenna attitude error
天线姿态误差
补充资料：定风波 商角调 商角调 西江客舍
【诗文】：
恨行云、特地高寒，牢笼好梦不定。婉娩年华，凄凉客况，泥酒浑成病。画阑深，碧窗静。一树瑶花可怜影。低映。怕月明照见，青禽相并。素衾自冷。又寒香、枕上薰愁醒。甚银床霜冻，山童未起，谁汲墙阴井。玉笙残，锦书迥。应是多情道薄＊。争肯。便等闲孤负，西湖春兴。
【注释】：
【出处】：
恨行云、特地高寒，牢笼好梦不定。婉娩年华，凄凉客况，泥酒浑成病。画阑深，碧窗静。一树瑶花可怜影。低映。怕月明照见，青禽相并。素衾自冷。又寒香、枕上薰愁醒。甚银床霜冻，山童未起，谁汲墙阴井。玉笙残，锦书迥。应是多情道薄＊。争肯。便等闲孤负，西湖春兴。
【注释】：
【出处】：
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条