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