Lagrange point orbit prediction using high-fidelity orbit propagator and orbit representation in rotating reference frame

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Authors: AMIT K. SINGH, Vineet K. Srivastava, Sonali Agarwal
Cited by: 2
References: 17

Fields of Study & Subjects

Spacecraft Dynamics and Control Space Satellite Systems and Control Numerical methods for differential equations

Publication details

Journal / source
Journal of Astrophysics and Astronomy
Publisher
Springer Science and Business Media LLC
Volume
47
Issue
1
Publication date
21 January 2026
Language
EN