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Space flight dynamics covers Keplerian mechanics for two-body problems, orbital maneuvers and maintenance, rendezvous and docking strategies, active debris removal, on-orbit servicing, formation flying missions, and interplanetary transfers. Orbital perturbations due to non-sphericity, aerodynamic drag, solar radiation pressure, and third body effects are analyzed. Key concepts include Hohmann and bielliptic transfer orbits for reaching targets like the ISS. Orbit determination using ground sensors is crucial. Relative motion and orbital perturbation methods are essential for accurate satellite behavior prediction.
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- Orbital dynamics and maneuvers: Keplerian mechanics are used for simplifying assumptions in two-body problems, with orbital perturbations affecting satellite behavior. Maneuvers include in-plane and out-of-plane adjustments, often impulsive for short durations.
- Hohmann and bielliptic transfers: techniques to change orbits, considering failure scenarios by adjusting the Soyuz orbit if necessary.
- Orbit determination and space situational awareness: using ground sensors and orbital mechanics to track objects in space, addressing risks from debris and fragments.
- Relative motion and satellite servicing: strategies for rendezvous, docking, active debris removal, on-orbit servicing, and formation flying missions involving multiple satellites.
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