AEE462 Lecture 4, Part A - Moving Elliptic Orbits in Time
We introduce Eccentric Anomaly and Mean Anomaly and show how to use Kepler's 2nd law to predict the position and velocity of a spacecraft or planet at any point in the future or the past.
We introduce Eccentric Anomaly and Mean Anomaly and show how to use Kepler's 2nd law to predict the position and velocity of a spacecraft or planet at any point in the future or the past.