Mode Analysis for Long-Term Behavior in a Resonant Earth-Moon Trajectory

被引：13
|
作者：
Short, Cody [1 ,4 ]
Howell, Kathleen [1 ]
Haapala, Amanda [3 ]
Dichmann, Donald [1 ,2 ]
机构：
[1] Purdue Univ, Sch Aeronaut & Astronaut, 701 West Stadium Ave, W Lafayette, IN 47907 USA
[2] NASA Goddard Space Flight Ctr, 8800 Greenbelt Rd, Greenbelt, MD 20771 USA
[3] Johns Hopkins Univ, Appl Phys Lab, Laurel, MD 20723 USA
[4] Analytical Graphics Inc, 220 Valley Creek Blvd, Exton, PA 19341 USA
来源：
JOURNAL OF THE ASTRONAUTICAL SCIENCES | 2017年 / 64卷 / 02期
关键词：
Multi-body dynamical systems; Ephemeris trajectory analysis; Cauchy-Green strain tensor; Finite-time Lyapunov exponent; Frequency analysis; Numerical perturbations; INVARIANT-MANIFOLDS; COHERENT STRUCTURES; ORBITS; PERTURBATIONS; EVOLUTION; DESIGN;
D O I：
10.1007/s40295-016-0098-9
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
Trajectory design in chaotic regimes allows for the exploitation of system dynamics to achieve certain behaviors. For example, for the Transiting Exoplanet Survey Satellite (TESS) mission, the selected science orbit represents a stable option well-suited to meet the mission objectives. Extended analysis of particular solutions nearby in the phase space reveals transitions into desirable terminal modes induced by natural dynamics. This investigation explores the trajectory behavior and borrows from flow-based analysis strategies to characterize modes of such a motion. Perturbed initial states from a TESS-like orbit are evolved to supply motion suitable for contingency analysis. Through the associated analysis, mechanisms are identified that drive the spacecraft into particular modes and supply conditions necessary for such transitions.
引用
收藏
页码：156 / 187
页数：32
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