Perturbing and Oblateness's Impact on the Generalized Photogravitational Restricted Three-Body Problem

In this research work, the effects of perturbing and oblateness on the generalised photogravitational restricted three body problem (RTBP) are examined when the primary are regarded as radiation sources and oblate spheroid. The perturbing forces were included in the equations of motion that we developed for the system. The triangular libration points were derived in terms of the perturbing parameters using linear approximations, and their influence was seen. Applying Murray's criteria, we determined that the triangular libration points remained unstable due to the nature of the characteristics equation matching to the variational equations of motion of the system generated.

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Publication Details

Journal
International Journal of Scientific Research in Science and Technology
Published
2024-09-30
DOI
https://doi.org/10.32628/ijsrst2411442
Primary Topic
Spacecraft Dynamics and Control
Type
article
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article

Perturbing and Oblateness's Impact on the Generalized Photogravitational Restricted Three-Body Problem

Avdhesh Kumar, Mahesh Kumar
International Journal of Scientific Research in Science and Technology
Spacecraft Dynamics and Control
article

Perturbing and Oblateness's Impact on the Generalized Photogravitational Restricted Three-Body Problem

Avdhesh Kumar, Mahesh Kumar
article en

Abstract

In this research work, the effects of perturbing and oblateness on the generalised photogravitational restricted three body problem (RTBP) are examined when the primary are regarded as radiation sources and oblate spheroid. The perturbing forces were included in the equations of motion that we developed for the system. The triangular libration points were derived in terms of the perturbing parameters using linear approximations, and their influence was seen. Applying Murray's criteria, we determined that the triangular libration points remained unstable due to the nature of the characteristics equation matching to the variational equations of motion of the system generated.

International Journal of Scientific Research in Science and TechnologyVol. 11(5)
Jai Prakash University (IN)
Openalex Percentile: Top 74%
Spacecraft Dynamics and Control
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