Chinese Space Science and Technology
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Che Rucai Zhang Honghua(Beijing Institute of Control Engineering,Beijing 100080)
Online:
Abstract: Firstly,the relative motion equation between the chaser and the non-cooperative target was presented in the form of orbit elements difference.Secondly,based on the measurement equations,a novel relative orbit determination method was proposed using two step estimation.The effectiveness of the proposed method was verified by the simulated experiment.
Che Rucai Zhang Honghua(Beijing Institute of Control Engineering,Beijing 100080). Investigation of Relative Orbit Determination Method for Tracking a Space Non-cooperative Target[J]. Chinese Space Science and Technology.
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https://journal26.magtechjournal.com/kjkxjs/EN/Y2007/V27/I04/7
