1·Attitude measurement was the measurement of attitude Angle.
姿态测量也就是对姿态角的测量。
2·The attitude Angle of high-speed mobile object in the shield tube is tested by use of optical lever in this paper.
采用光学杠杆的方法对遮蔽管内的高速运动物体进行姿态角测试。
3·After analysed recognition criteria, an horizon detection algorithm and transform formula for attitude Angle are attained.
文中给出了地平线判别准则及相应的算法和姿态角变换公式。
4·In this paper a method for measuring the relative position and attitude Angle of the spacecraft during rendezvous and docking.
本文叙述了一种测量空间飞行器交会对接过程中位置和姿态角的方法。
5·The attitude Angle (or angular rate) data of INS were often ignored during study and application of automatic alignment technique.
在以往的自对准技术研究与应用中，惯导系统的姿态角(或角速率)信息往往是被忽略不用的。
6·A method to limit the amplification in a certain range is proposed for restricting the big estimated error of pitch attitude angle.
本文还提出了限定增益系数的方法，以抑制俯仰角过大的估计误差。
7·The composition and principle of the platform were introduced, and the error equations of attitude Angle, velocity and position were given.
介绍了平台的组成及工作原理，并且推导出平台角误差方程、速度误差方程和位置误差方程。
8·Compared with the whole attitude Angle matching recognition methods, the proposed method need small memory space and small calculation time.
与一维距离像全姿态角匹配识别方法比较，具有计算量、存贮量较小的特点。
9·The method is simple, requires little computation. the relative position and attitude Angle of the trace spacecraft can be given through measuring.
这种方法简单所需的运算量也较少，通过测量能给出追踪飞行器相对于目标飞行器的位置和姿态角。
10·There are many methods to measurement the flying attitude, such as solar attitude angle sensor, high-speed photography and geomagnetic field sensor.
飞行体的姿态测试方法有许多种，如太阳方位角传感器遥测、高速摄影法、地磁传感器等。