首页> 外文会议>Saint Petersburg International Conference on Integrated Navigation Systems; 20040524-26; Saint Petersburg(RU) >IN-FLIGHT CALIBRATION OF THE ESG-BASED SPACECRAFT ATTITUDE REFERENCE SYSTEM USING A STELLAR SENSOR
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IN-FLIGHT CALIBRATION OF THE ESG-BASED SPACECRAFT ATTITUDE REFERENCE SYSTEM USING A STELLAR SENSOR

机译:使用恒星传感器的基于ESG的航天飞机姿态参考系统的飞行中校准

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摘要

An algorithm based on the data from the SIARS and the spacecraft stellar sensor, using the generalized Kalman filler, has been developed. The algorithm provides refinement of the SIARS ESG drift model coefficients after the spacecraft is placed in orbit, as well as estimation of errors in referencing the IMU axes to the axes of the stellar sensor. The errors of the integrated system become observable through the measurements of the spacecraft rolling angles.
机译:已经开发了一种基于SIARS和航天器恒星传感器的数据的算法,并使用了广义的Kalman填料。该算法提供了航天器进入轨道后SIARS ESG漂移模型系数的细化,以及将IMU轴参考恒星传感器的轴时的误差估计。通过测量航天器的滚动角,可以观察到集成系统的误差。

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