During atmospheric re-entry of rocket sub-stages, GNSS signals may be lost for extended periods due to plasma sheath and attitude occlusion. In such scenarios, the integrated navigation system degrades to pure inertial navigation, and position errors grow cubically over time, making conventional filtering and predictio...
Tao-Ran Xu, Jing Yang, Kang Wang et al.· Journal of Physics, Conferen...· 0 citations
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