AEE462 Lecture 5, Part A - Moving Hyperbolic Orbits in Time
We repeat Lecture 4 in the case of Hyperbolic Trajectories (Orbits). We define Hyperbolic anomaly, hyperbolic Mean Anomaly, and a hyperbolic Kepler's Equation. This can be used to predict future position and velocity. We also consider a Jupiter flyby example. (FYI: Unfortunately, because I forgot to multiply by 2 in this last example, the spacecraft did not survive...)