Cubesat Deployment from a Near Rectilinear Halo Orbit

Mapping Intimacies ◽

10.2514/6.2022-1777 ◽

2022 ◽

Author(s):

Diane C. Davis ◽

Emily M. Zimovan-Spreen ◽

Rolfe J. Power ◽

Kathleen C. Howell

Keyword(s):

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

Acta Astronautica ◽

10.1016/j.actaastro.2011.05.017 ◽

2011 ◽

Vol 69 (9-10) ◽

pp. 882-891 ◽

Author(s):

Majid Salmani ◽

Christof Büskens

Keyword(s):

Real Time ◽

Body Problem ◽

The Sun ◽

Real Time Control ◽

Time Control ◽

Four Body Problem

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Moon’s Influence on the Transfer from the Earth to a Halo Orbit Around L 1

Predictability, Stability, and Chaos in N-Body Dynamical Systems - NATO ASI Series ◽

10.1007/978-1-4684-5997-5_23 ◽

1991 ◽

pp. 283-290 ◽

Author(s):

Gerard Gómez ◽

Àngel Jorba ◽

Josep Masdemont ◽

Carles Simó

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Radii in the sd shell and the 1s 1/2 “halo” orbit: A game changer

Journal of Physics Conference Series ◽

10.1088/1742-6596/1023/1/012016 ◽

2018 ◽

Vol 1023 ◽

pp. 012016 ◽

Author(s):

J. Bonnard ◽

A. P. Zuker

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Spacecraft Rendezvous Utilizing Invariant Manifolds for a Halo Orbit

TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES ◽

10.2322/tjsass.58.261 ◽

2015 ◽

Vol 58 (5) ◽

pp. 261-269 ◽

Author(s):

Yuki SATO ◽

Kenji KITAMURA ◽

Takeya SHIMA

Keyword(s):

Invariant Manifolds ◽

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Near Rectilinear Halo Orbit Determination with Simulated DSN Observations

AIAA Scitech 2020 Forum ◽

10.2514/6.2020-1700 ◽

2020 ◽

Author(s):

Nathan L. Parrish ◽

Matthew J. Bolliger ◽

Ethan Kayser ◽

Michael R. Thompson ◽

Jeffrey S. Parker ◽

...

Keyword(s):

Orbit Determination ◽

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Transfer From the Earth to a Halo Orbit

Dynamics and Mission Design Near Libration Points - World Scientific Monograph Series in Mathematics ◽

10.1142/9789812794628_0004 ◽

2001 ◽

pp. 93-126 ◽

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THE SOHO MISSION L1 HALO ORBIT RECOVERY FROM THE ATTITUDE CONTROL ANOMALIES OF 1998

Libration Point Orbits and Applications ◽

10.1142/9789812704849_0009 ◽

2003 ◽

Author(s):

C.E. ROBERTS

Keyword(s):

Attitude Control ◽

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Linear Quadratic Formulation based Station-Keeping in Halo Orbit

2019 Sixth Indian Control Conference (ICC) ◽

10.1109/icc47138.2019.9123220 ◽

2019 ◽

Author(s):

Ramteke Vivek Haribhau ◽

Shashi Ranjan Kumar

Keyword(s):

Station Keeping ◽

Linear Quadratic

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Trajectory determination support and analysis for ISEE-3 from halo orbit to escape from the earth/moon system

10.2514/6.1984-1980 ◽

1984 ◽

Author(s):

J. JOYCE ◽

A. SCHANZLE

Keyword(s):

Moon System ◽

The Earth ◽

Trajectory Determination

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Halo orbit mission correction maneuvers using optimal control

10.1016/s0005-1098(01)00279-5 ◽

2002 ◽

Vol 38 (4) ◽

pp. 571-583 ◽

Author(s):

Radu Serban ◽

Wang S. Koon ◽

Martin W. Lo ◽

Jerrold E. Marsden ◽

Linda R. Petzold ◽

...

Keyword(s):

Optimal Control ◽

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