Port-Hamiltonian Based Control of the Sun-Earth 3D Circular Restricted Three-Body Problem: Stabilization of the <i>L</i><sub>1</sub> Lagrange Point

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ISSN Print: 2164-0165
ISSN Online: 2164-0181
www.scirp.org/journal/mme
E-mail: mme@scirp.org

"Port-Hamiltonian Based Control of the Sun-Earth 3D Circular Restricted Three-Body Problem: Stabilization of the L₁ Lagrange Point"
written by Haotian Yan,
published by Modern Mechanical Engineering, Vol.10 No.3, 2020

has been cited by the following article(s):

[1]	The Coupling Orbit–Attitude–Structure Evolution of Rubble-Pile Asteroid with Earth Flyby in the Restricted Three-Body Problem
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[2]	The Coupling Orbit–Attitude–Structure Evolution of Rubble-Pile Asteroid with Earth Flyby in the Restricted Three-Body Problem. Aerospace 2022, 9, 351
	2022

[1]	Non-linear dynamics of a test particle near the Lagrange points L4 and L5 (Earth-Moon and Sun-Earth case) EUREKA: Physics and Engineering, 2024 DOI:10.21303/2461-4262.2024.002949

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[3]	A study of the nonlinear dynamics inside the exoplanetary system Kepler-22 using MATLAB® software EUREKA: Physics and Engineering, 2024 DOI:10.21303/2461-4262.2024.003257

[4]	Trajectory tracking PID passivity-based control of spacecraft formation flying around Sun-Earth L2 point in the port-Hamiltonian framework Advances in Space Research, 2024 DOI:10.1016/j.asr.2024.07.054

[5]	The Coupling Orbit–Attitude–Structure Evolution of Rubble-Pile Asteroid with Earth Flyby in the Restricted Three-Body Problem Aerospace, 2022 DOI:10.3390/aerospace9070351

[6]	The Coupling Orbit–Attitude–Structure Evolution of Rubble-Pile Asteroid with Earth Flyby in the Restricted Three-Body Problem Aerospace, 2022 DOI:10.3390/aerospace9070351

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