The book link is httpsdrivegooglecomopenid0B8HzyF8RfYSTMkpzb

The book link is   https://drive.google.com/open?id=0B8HzyF8RfYSTMkpzbjNiTFJiRFE

Simulate the satellite motion including Moon\'s gravity effect. This is not a two-body problem since we have another body (Moon). Please, refer to the restricted three-body problem (Sec. 2.12 of our textbook). 1. You need to generate the two plots. One is the satellite orbit in the barycentric co-moving frame for Earth-Moon system. The other is the same satellite orbit in ECIF frame. 2. Derive a coordinate transformation from the barycentric frame to ECIF. 3. Attach MATLAB codes.

Solution

https://drive.google.com/open?id=0B8HzyF8RfYSTMkpzbjNiTFJiRFE