Real-time control of optimal low-thrust transfer to the Sun–Earth L1 halo orbit in the bicircular four-body problem-Reference-Cited by-同舟云学术

Real-time control of optimal low-thrust transfer to the Sun–Earth L1 halo orbit in the bicircular four-body problem

Published:2011-11 Issue:9-10 Volume:69 Page:882-891
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Salmani Majid,Büskens Christof

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference35 articles.

1. Trajectories and orbital maneuvers for the first libration-point satellite;Farquhar;Journal of Guidance and Control,1980

2. R.W. Farquhar, The Control and Use of Libration-Point Satellites, Ph.D. Dissertation, Department of Aeronautics and Astronautics, Stanford University, Stanford, CA, 1968.

3. Stationkeeping method for libration point trajectories;Howell;Journal of Guidance and Control,1993

4. On the optimal station keeping control of halo orbits;Sim;Acta Astronautica,1987

5. Invariant manifolds, the spatial three-body problem and space mission design;Gómez;Advances in Astronautical Sciences,2001

Cited by 9 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Trajectory correction for lunar flyby transfers to libration point orbits using continuous thrust;Astrodynamics;2021-02-01

2. Families of Earth–Moon trajectories with applications to transfers towards Sun–Earth libration point orbits;Astrophysics and Space Science;2019-03

3. Study of Correction Maneuver for Lunar Flyby Transfers in the Real Ephemeris;Journal of Guidance, Control, and Dynamics;2018-10

4. Parametric stability analysis for planar bicircular restricted four-body problem;Astrodynamics;2018-05-15

5. Study of Time-Free Transfers into Libration Point Orbits with Multiple Constraints;Journal of Guidance, Control, and Dynamics;2017-11