摘要
Currently, the deep space explorer formation fight is a novel area of aerospace technique [15]. The formation fight can increase redundancy backup, decentralize the cost, and provide a multi-platform for the deep space exploration [17]. For the deep space explorer formation fight, both absolute and relative navigation accuracies are crucial, especially the relative one. Orbit determination of a spacecraft is primarily performed at a ground station [4]. Unfortunately, subject to the long distance between the explorer and the earth, traditional ground station-based navigation methods cannot provide high-accuracy and real-time navigation information. Consequently, the autonomous navigation systems [12], [13], which observe the celestial bodies to obtain the navigation information, are highly attractive.
| 源语言 | 英语 |
|---|---|
| 文章编号 | 7081637 |
| 页(从-至) | 30-39 |
| 页数 | 10 |
| 期刊 | IEEE Aerospace and Electronic Systems Magazine |
| 卷 | 30 |
| 期 | 3 |
| DOI | |
| 出版状态 | 已出版 - 1 3月 2015 |
学术指纹
探究 'X-ray pulsar/starlight Doppler integrated navigation for formation flight with ephemerides errors' 的科研主题。它们共同构成独一无二的学术指纹。引用此
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