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AEE462 Lecture 5, Part A - Moving Hyperbolic Orbits in Time
Автор: Cybernetic Systems and Controls
Загружено: 2021-02-02
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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...)
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