Libration Transfer Design Using Patched Elliptic Three-Body Models and Graphics Processing Units-Reference-Cited by-同舟云学术

Libration Transfer Design Using Patched Elliptic Three-Body Models and Graphics Processing Units

Published:2017-12 Issue:12 Volume:40 Page:3155-3166
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Peng Hao¹,Bai Xiaoli¹,Masdemont Josep J.²,Gómez Gerard³,Xu Shijie⁴

Affiliation:

1. Rutgers, The State University of New Jersey, New Brunswick, New Jersey 08854

2. Polytechnic University of Catalonia, 08034 Barcelona, Spain

3. University of Barcelona, 08007 Barcelona, Spain

4. Beihang University, 100083 Beijing, People’s Republic of China

Funder

Air Force Office of Scientific Research

Office of Naval Research

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Link

https://arc.aiaa.org/doi/am-pdf/10.2514/1.G002692

Reference30 articles.

1. CanaliasA. E.GómezG.MarcoteM.MasdemontJ. J. “Assessment of Mission Design Including Utilization of Libration Points and Weak Stability Boundaries,” ESA Advanced Concept Team TR 18142/04/NL/MV, 2004.

2. Application of dynamical systems theory to trajectory design for a libration point mission

3. Study of the transfer from the Earth to a halo orbit around the equilibrium pointL 1

4. Analysis of Capture Trajectories into Periodic Orbits About Libration Points

5. Analysis of Two-Impulse Capture Trajectories into Halo Orbits of Sun–Mars System

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