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Jianfeng Yin

China Academy of Space Technology

6

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19

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A linear model for relative motion in an elliptical orbit based on a spherical coordinate system

2019 Acta Astronautica
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Algorithm of Relative Lambert Transfer Based on Relative Orbital Elements

2019 Journal of Guidance Control and Dynamics
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Spacecraft Fast Fly-Around Formations Design Using the Bi-Teardrop Configuration

2018 Journal of Guidance Control and Dynamics
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Relative Lambert Transfer for Elliptical Reference Orbit Based on Relative Orbit Elements

2016
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Hovering Formation Design and Control Based on Relative Orbit Elements

2016 Journal of Guidance Control and Dynamics
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Inverse Transformation of Elliptical Relative State Transition Matrix

2014 International Journal of Astronomy and Astrophysics
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