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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 core of stabilization platform is the attitude measurement and control of the carrier.

稳定平台的核心问题是载体姿态测量和控制技术。

3·There are mostly two models in attitude measurement: cumulative model and unfolding model.

态度测量主要应用两种模型：累进型与展开型。

4·Test results show that these methods significantly improve the attitude measurement precision.

误差实验结果表明，该补偿方法可以提高姿态测量的精度。

5·The test results show the feasibility of the exterior attitude measurement based on linear CCD.

测试结果表明，这个基于线阵CCD的外姿态测量方法是可行的。

6·The errors of heading and attitude measurement with GPS are discussed and the schemes are proposed.

通过误差分析，讨论了影响GPS航姿测定的各项误差，提出了GPS航姿测量方案。

7·An attitude measurement approach for micro air vehicles (MAVs) based on image information was presented.

提出了一种基于图像信息的微小型飞行器姿态测量方法。

8·Star sensor is a high-precision, high reliability attitude measurement equipment of astronomical navigation system.

星敏感器是天文导航系统的主要设备，是一种高精度、高可靠性的姿态测量部件。

9·The attitude of the carrier is obtained by further using an attitude measurement algorithm through the fixed solutions.

通过固定解进一步利用姿态测量算法得到载体的姿态。

10·Abstract: a method based on optimization functions was proposed to improve the attitude measurement precision of a plane.

摘要：提出了基于构建最优函数来提高飞机姿态测量精度的方法。