Canonical Modelling of Relative Spacecraft Motion Via Epicyclic Orbital Elements
- 作者N. Jeremy Kasdin; Pini Gurfil; Egemen Kolemen
- 卷第92卷
- 期第4期
- 印刷ISSN0923-2958
- 电子ISSN1572-9478
- 文件大小891.69KB
- 发表时间2005-08
- DOI10.1007/s10569-004-6441-7
- 页码337-370
The Relative Lyapunov Indicator: An Efficient Method of Chaos DetectionZsolt Sándor; Bálint Érdi; András Széll; Barbara Funk · 2004
Stability of higher order resonances in the restricted three-body problemBálint Érdi, Renáta Rajnai, Zsolt Sándor, Emese Forgács-Dajka · 2012
The Phase Space Structure Around L4 in the Restricted Three-Body ProblemZsolt Sándor; Bálint Érdi; Christos Efthymiopoulos · 2000
Short Time Lyapunov Indicators in the Restricted Three-Body ProblemZsolt Sàndor; Róbert Balla; Ferenc Téger; Bálint Érdi · 2001
Symplectic Mappings of Co-orbital Motion in the Restricted Problem of Three BodiesZsolt Sándor; Bálint Érdi; Carl D. Murray · 2002
Symplectic Mapping for Trojan-Type Motion in the Elliptic Restricted Three-Body ProblemZsolt Sándor; Bálint Érdi · 2003