提出了一种基于图像信息的微小型飞行器姿态测量方法。
An attitude measurement approach for micro air vehicles (MAVs) based on image information was presented.
CCD星跟踪器作为飞行器的姿态测量仪器有许多优点，它必须有一种全天自主星图识别算法来支持其工作。
As a spacecraft attitude measurement instrument, CCD star tracker has a lot of advantages. But it needs an all-sky autonomous star map identification algorithm to support its operation.
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。
In this paper a method for measuring the relative position and attitude Angle of the spacecraft during rendezvous and docking.
星敏感器是为空间飞行器姿态控制系统提供姿态信息的测量系统。
The star sensor is a measuring unit used for providing information to the attitude control system on spacecraft .
要实现在真实飞行情况下对微型飞行器姿态等数据的测量，数据的无线收发是其关键技术。
To get the data of the micro air vehicle (MAV) 's attitude in true flight, the data transmit and receive equipment is the key technology.
飞行器制导精度评估，特别是航天器的姿态与定点控制、落点预报等，都离不开高精度的外弹道测量数据。
Assessing the accuracy of guidance system, especially controlling of missile's attitude and station keeping maneuver and landing point forecasting all rely on the reliable trajectory measurement.
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。
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。
The method is simple, requires little computation. the relative position and attitude Angle of the trace spacecraft can be given through measuring.
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