1–19 von 19 Ergebnissen
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    Aerogravity-assist capture into the three-body system: A preliminary design

    Han, Hongwei / Li, Xiangyu / Qiao, Dong | Elsevier | 2022

    A LSTM assisted orbit determination algorithm for spacecraft executing continuous maneuver

    Zhou, Xingyu / Qin, Tong / Ji, Mingjiang et al. | Elsevier | 2022

    An adaptive surrogate model-based fast planning for swarm safe migration along halo orbit

    Zhou, Xingyu / Cheng, Yu / Qiao, Dong et al. | Elsevier | 2022

    Analysis of the solar sail deformation based on the point cloud method

    Huang, Xiyao / Zeng, Xiangyuan / Circi, Christian et al. | Elsevier | 2020

    Cislunar L 4 and L 5 axial orbits and their applications

    Qiao, Dong / Zheng, Jianchao / Qi, Yi | Elsevier | 2024

    Design and analysis of an extended mission of CE-2: From lunar orbit to Sun–Earth L2 region

    Qiao, Dong / Cui, Pingyuan / Wang, Yamin et al. | Elsevier | 2013

    Design of optimal impulse transfers from the Sun–Earth libration point to asteroid

    Wang, Yamin / Qiao, Dong / Cui, Pingyuan | Elsevier | 2015

    Landing of hopping rovers on Irregularly-shaped small bodies using attitude control

    Li, Xiangyu / Sanyal, Amit K. / Warier, Rakesh R. et al. | Elsevier | 2020

    Proposal for a multiple-asteroid-flyby mission with sample return

    Qiao, Dong / Cui, Pingyuan / Cui, Hutao | Elsevier | 2012

    Semi-analytical configuration optimization of geocentric gravitational wave observatory

    Jia, Feida / Li, Xiangyu / Qiao, Dong et al. | Elsevier | 2022

    The design of transfer trajectory for Ivar asteroid exploration mission

    Qiao, Dong / Cui, Hutao / Cui, Pingyuan | Elsevier | 2009