JOURNAL BROWSE
Search
Advanced SearchSearch Tips
Comparison of Global Optimization Methods for Insertion Maneuver into Earth-Moon L2 Quasi-Halo Orbit Considering Collision Avoidance
facebook(new window)  Pirnt(new window) E-mail(new window) Excel Download
 Title & Authors
Comparison of Global Optimization Methods for Insertion Maneuver into Earth-Moon L2 Quasi-Halo Orbit Considering Collision Avoidance
Lee, Sang-Cherl; Kim, Hae-Dong; Yang, Do-Chul; Cho, Dong-Hyun; Im, Jeong-Heum; No, Tae-Soo; Kim, Seungkeun; Suk, Jinyoung;
  PDF(new window)
 Abstract
A spacecraft placed in an Earth-Moon L2 quasi-halo orbit can maintain constant communication between the Earth and the far side of the Moon. This quasi-halo orbit could be used to establish a lunar space station and serve as a gateway to explore the solar system. For a mission in an Earth-Moon L2 quasi-halo orbit, a spacecraft would have to be transferred from the Earth to the vicinity of the Earth-Moon L2 point, then inserted into the Earth-Moon L2 quasi-halo orbit. Unlike the near Earth case, this orbit is essentially very unstable due to mutually perturbing gravitational attractions by the Earth, the Moon and the Sun. In this paper, an insertion maneuver of a spacecraft into an Earth-Moon L2 quasi-halo orbit was investigated using the global optimization algorithm, including simulated annealing, genetic algorithm and pattern search method with collision avoidance taken into consideration. The result shows that the spacecraft can maintain its own position in the Earth-Moon L2 quasi-halo orbit and avoid collisions with threatening objects.
 Keywords
Circular Restricted Three Body Problem;Quasi-Halo;Collision Avoidance;Space Objects;Simulated Annealing;Genetic Algorithm;Pattern Search;Maneuver Planning;Orbit Insertion Maneuver;
 Language
English
 Cited by
1.
원형 제한 3체 문제의 불변위상공간을 이용한 행성간 궤적설계 기초 연구,정옥철;안상일;정대원;김은규;방효충;

한국항공우주학회지, 2015. vol.43. 8, pp.692-698 crossref(new window)
 References
1.
Dawn Perry Gordon., Transfers to Earth-Moon L2 HALO Orbits Using Lunar Proximity and Invariant Manifolds, M.S. Thesis, Purdue University, August 2008.

2.
Bernelli F, Topputo F. and Massari M., Assessment of Mission Design Including Utilization of Libration Points and Weak Stability Boundaries, Final Report, ESTEC Contract No. 18147/04/NL/MV, 2004.

3.
http://en.wikipedia.org/wiki/Lagrangian_point

4.
Woodard, M., Folta, D., and Woodfork, D., "ARTEMIS: The First Mission to the Lunar Libration Points", presented at the 21st International Symposium on Space Flight Dynamics (ISSFD), Toulouse, France, September 28 - October 2, 2009.

5.
http://www.answers.com/topic/space-exploration

6.
dos Santos, D.P.S., and Prado, A.F.B.A., Minimum Fuel Multi-Impulsive Orbital Maneuvers Using Genetic Algorithms, IAA-AAS-DyCoSS1-11-01.

7.
Michael A. Paluszek, and Stephanie J. Thomas, "Trajectory Optimization Using Global Methods", The 29th International Electric Propulsion Conference Princeton University, October 31 - November 4, 2005.

8.
Lu-sha Wang, Zhi-gang Wang, and Wei Li, Optimization of Parameters Injecting into Orbits Based on the Pattern Search Method, 2009 First International Conference on Information Science and Engineering(ICISE), 2009, pp.3823-3826.

9.
Willem H. de Vries, Maneuver Optimization through Simulated Annealing, Lawrence Livermore National Laboratory, LLNL-CONF-497728.

10.
Hae-Dong Kim, and Eun-Sum Sim, "Lunar Transfer Trajectory Design Using a WSB", Proceeding of the 2009 KSAS Fall Conference, 2009. 21-1201.

11.
Michael A. Paluszek, and Stephanie J. Thomas, "Trajectory Optimization Using Global Methods", The 29th International Electric Propulsion Conference Princeton University, October 31 - November 4, 2005.

12.
MATLAB, Global Optimization ToolBox, Mathworks.

13.
Sang-Cherl Lee, Hae-Dong Kim, and Jinyoung Suk, "Collision Avoidance Maneuver Planning Using GA for LEO and GEO Satellite Maintained in Keeping Area", Int'l J. of Aeronautical & Space Sci., Vol. 13, No.4, 2012, pp. 474-483. crossref(new window)

14.
Magnus Erik Hvass Pedersen, Tuning & Simplifying Heuristical Optimization, Ph.D. Thesis for the degree of Doctor of Philosophy, January 2010

15.
Rosario Laureano, Determinism Versus Predictability in the Context of Poincare's Work on the Restricted 3-Body Problem, University Institute of Lisbon, Portugal, Vol. 2, No. 2, March 2012.ISSN-L: 2223-9553, ISSN: 2223-9944.

16.
Pierpaolo Pergola, Chiara Finocchietti, "Circular Restricted Tree Body Model", Space System Lecture, Pisa, November 2012.

17.
F.Renk, M.Landgraf, "Sun-Earth Libration point transfer options with intermediate HEO", ActaAstronautica, Vol. 74, May-June 2012, pp. 1-19. crossref(new window)

18.
Infeld, Samantha I., Optimization of mission design for constrained libration point space missions, ProQuest Dissertations And Theses; Thesis (Ph.D.), Stanford University, 2006, Publication Number: AAI3209042; ISBN: 9780542570926; Source: Dissertation Abstracts International, Volume: 67-02, Section: B, page: 1001.; 133 p.

19.
Tae Soo No, JiMarn Lee, Gyeong Eon Jeon, Daero Lee, and Ghangho Kim, "A Study on Earth-Moon Transfer Orbit Design", Int'l J. of Aeronautical & Space Sci., Volume 13, No. 1, 2012, pp. 106-116. crossref(new window)

20.
Parker, Jeff., Dynamical Systems Theory Applied to Spacecraft Mission Design, Dec 6, 2012.

21.
Kyle Wolma, The Use of Lagrange Points for Lunar Exploration, Settlement, and Support, ASEN5050, Colorado University.

22.
STK Tutorial, Trajectory Design with STK/Astorgator : Earth-Moon L1 Trajectory Tutorial.

23.
Alfano, S., "A Numerical Implementation of Spherical Object Collision Probability", The Journal of Astronautical Sciences, Vol. 53, No. 1, January-March 2005, pp. 103-109.

24.
Michael R. Phillips, Spacecraft Collision Probability Estimation For Rendezvous and Proximity and Operation, Utah State University, 2012.

25.
Alfano S, "Collision avoidance maneuver planning tool", in Proceedings of the 15th AAS/AIAA Astrodynamics Specialist Conference, Lake Tahoe, CA, 7-11 Aug 2005.

26.
Alfano S, "Review of conjunction probability methods for short-term encounters", in Proceedings of the AAS/AIAA Space Flight Mechanics Meeting, Sedona, AZ, 28 Jan-1 Feb 2007.

27.
Eun-Hyouek Kim, Hae-Dong Kim, Hak-Jung Kim, "Optimal Solution of Collision Avoidance Maneuver with Multiple Space Debrisc, Journal of Space Operations-Letters, Vol. 9, No. 3, July-September 2012.