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.2021.111387Additional 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.