To model the effects of orbital perturbations caused by gravitational asymmetry due to oblateness and presence of a third body.

    To present a simple atmospheric model for predicting the life of a satellite in a low orbit.

    To introduce the concept of sphere of influence and the patched conic approach for the design and analysis of lunar and interplanetary missions.

    To solve the perturbed two-body problem using numerical integration (Cowell’s and Encke’s methods).


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    Analytic formulation for J2 perturbed orbits

    Sgubini, Silvano / Palmerini, Giovanni B. | TIBKAT | 2023

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    J2-PERTURBED LOW-ENERGY ORBITS AROUND ENCELADUS

    Alkhaja, Adham / Salazar, Francisco / Fantino, Elena et al. | TIBKAT | 2021



    Nonlinear Uncertainty Propagation for Perturbed Two-Body Orbits

    Vishwajeet, Kumar / Singla, Puneet / Jah, Moriba | AIAA | 2014