用于自由飞行机器人和陆地测量卫星的天体惯性姿态确定系统的飞行校准、对准和验证

Y. Somov, S. Butyrin, S. Somov, T. Somova
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引用次数: 10

摘要

本文研究了在550 ~ 1000 km轨道高度上运行的自由飞行机器人和机动地面测量小卫星的精确姿态确定的一些主要问题。针对捷联惯导系统中的星惯姿态确定系统,提出了星惯姿态确定系统信号处理、标定、对准和验证的机载离散算法。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
In-flight calibration, alignment and verification of an astroinertial attitude determination system for free-flying robots and land-survey satellites
We consider some principal problems on precise attitude determination of the free-flying robots and maneuvering land-survey mini-satellites operated on the orbit altitudes from 550 up to 1000 km. We present onboard discrete algorithms for signal processing, calibration, alignment and verification of an astroinertial attitude determination system which is a part of the strapdown inertial navigation system.
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