Autonomous navigation method of high elliptical orbit satellite based on celestial navigation/accelerometer

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[1] [1,Wang, Peng
[2] Zhang, Ying-Chun
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Wang, Peng | 1600年 / Editorial Department of Journal of Chinese Inertial Technology卷 / 22期
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D O I：
10.13695/j.cnki.12-1222/o3.2014.04.019
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