We resumed today with orbital mechanics. We covered the two-body problem, introduced Kepler’s problem (time doesn’t relate well to true anomaly), and sprinted to the state transition matrix. We will resume with perturbations and additional bodies considered on Friday.

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Slides: L4 Slides – Two Body Problem

Previous lectures:

• L3 – Problem Solution and Review
• L2 – Orbital Mechanics Concepts
• L1 – Orbit Determination Concepts