Published November 2021 | Version v1
Journal article

Controlling the libration point orbits for CRTBP with non-ideal solar sail and albedo effect

  • 1. Department of Mathematics and Computing Indian Institute of Technology (ISM), Dhanbad 826004, Jharkhand (India)
  • 2. Department of Mathematics, C S A Govt. Lead College Sehore, MP (India)

Description

Libration point orbits around collinear points present numerous properties which are worthwhile for space missions. Because orbits around these points are exponentially unstable, station-keeping strategies aim for periodic motion.This paper considers the problem of Lagrangian point stabilisation in the Sun-Jupiter system with non-ideal solar sail and albedo effect. Energy shaping and dissipation injection are used to stabilize the Lagrangian points, which are originally unstable. Through shaping of Hamiltonian (energy) and dissipation injection at the designed equilibrium point, we obtained that a closed-loop system is stable and asymptotic stable respectively. We discover that the orbits are stable under port- Hamiltonian control using best fit results.

Availability note (English)

Available from http://dx.doi.org/10.1016/j.chaos.2021.111387

Additional details

Identifiers

DOI
10.1016/j.chaos.2021.111387;
PII
S0960077921007414;

Publishing Information

Journal Title
Chaos, Solitons and Fractals
Journal Volume
152
Journal Page Range
vp.
ISSN
0960-0779

INIS

Country of Publication
United Kingdom
Country of Input or Organization
International Atomic Energy Agency (IAEA)
INIS RN
53100309
Subject category
S97: MATHEMATICAL METHODS AND COMPUTING;
Descriptors DEI
ASYMPTOTIC SOLUTIONS; CONTROL; DESIGN; EQUILIBRIUM; HAMILTONIANS; LAGRANGIAN FUNCTION
Descriptors DEC
FUNCTIONS; MATHEMATICAL OPERATORS; MATHEMATICAL SOLUTIONS; QUANTUM OPERATORS

Optional Information

Copyright
Copyright (c) 2021 Elsevier Ltd. All rights reserved.