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Leveraging quasi-periodic orbits for trajectory design in cislunar space
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作者 brian p.mccarthy Kathleen C.Howell 《Astrodynamics》 CSCD 2021年第2期139-165,共27页
Incorporating quasi-periodic orbits into the preliminary design process offers a wide range of options to meet mission constraints and address the challenges in a complex trade space.In this investigation,linear stabi... Incorporating quasi-periodic orbits into the preliminary design process offers a wide range of options to meet mission constraints and address the challenges in a complex trade space.In this investigation,linear stability and quasi-periodic orbit family continuation schemes are examined to meet various types of constraints.Applications in eclipse avoidance and transfer design are examined by leveraging quasi-periodic orbits and their associated hyperbolic manifolds in the lunar region.Solutions are transitioned to an ephemeris model to validate that geometries are maintained in higher-fidelity models.When the natural dynamical structures associated with quasi-periodic orbits are leveraged,novel trajectory solutions can emerge. 展开更多
关键词 multi-body dynamical systems quasi-periodic orbits trajectory analysis cislunar trajectory design near rectilinear halo orbit ephemeris dynamical model
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