Broad search for unstable resonant orbits in the planar circular restricted three-body problem

被引：0
作者：
Rodney L. Anderson
Stefano Campagnola
Gregory Lantoine
机构：
[1] California Institute of Technology,Jet Propulsion Laboratory
[2] Japan Aerospace Exploration Agency,Department of Space Flight Systems, Institute of Space and Astronautical Science
来源：
Celestial Mechanics and Dynamical Astronomy | 2016年 / 124卷
关键词：
Resonant orbits; Dynamical systems theory; Orbit families; Continuation Three-body problem; Stability; CWIC;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
Unstable resonant orbits in the circular restricted three-body problem have increasingly been used for trajectory design using optimization and invariant manifold techniques. In this study, several methods for computing these unstable resonant orbits are explored including grid searches, flyby maps, and continuation. Families of orbits are computed focusing on orbits with multiple loops near the secondary in the Jupiter–Europa system, and their characteristics are explored. Different parameters such as period and stability are examined for each set of resonant orbits, and the continuation of several specific orbits is explored in more detail.
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页码：177 / 199
页数：22
相关论文
共 65 条
[1]  
Anderson RL(2015)Approaching Moons from resonance via invariant manifolds J. Guid. Control Dyn. 38 1097-1109
[2]  
Anderson RL(2009)Role of invariant manifolds in low-thrust trajectory design J. Guid. Control Dyn. 32 1921-1930
[3]  
Lo MW(2010)Dynamical systems analysis of planetary flybys and approach: planar Europa orbiter J. Guid. Control Dyn. 33 1899-1912
[4]  
Anderson RL(2011)A dynamical systems analysis of planetary flybys and approach: ballistic case J. Astronaut. Sci. 58 167-194
[5]  
Lo MW(2002)Spatial p-q resonant orbits of the RTBP Celest. Mech. Dyn. Astron. 84 387-407
[6]  
Anderson RL(2003)Three-dimensional p-q resonant orbits close to second species solution Celest. Mech. Dyn. Astron. 85 145-174
[7]  
Lo MW(2004)A note on second species solutions generated from p-q resonant orbits Celest. Mech. Dyn. Astron. 88 229-244
[8]  
Barrabés E(1995)Targeting chaotic orbits to the Moon through recurrence Phys. Lett. A 204 373-378
[9]  
Gómez G(2006)Nonplanar second species periodic and chaotic trajectories for the circular restricted three-body problem Celest. Mech. Dyn. Astron. 94 433-449
[10]  
Barrabés E(2000)Periodic and chaotic trajectories of the second species for the n-centre problem Celest. Mech. Dyn. Astron. 77 49-75
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