Problem 45812. SatCom #10: Rate of Precesion of Orbit Plane (Nodal Precession)
Solution Stats
Problem Comments

3 Comments
Nice problem group. The descriptions for the satellite orbit problems were quite technical, and some further intermediate problems to build on later would've been nice (e.g. the orbital period of a satellite in an elliptical orbit), but still  good one!
Tip: It is easy to miss the words "degrees per day" in the problem description.
Be aware that if you plan on calling the function developed in Problem 5 from Problem 10 then you must change the radius of the earth.
In Problem 5 the earth radius used is 6371 k m; = 6371000 m
In Problem 10 the earth radius used is 6378137 m;
Solution Comments
Show commentsProblem Recent Solvers22
Suggested Problems

How to find the position of an element in a vector without using the find function
2697 Solvers

498 Solvers

489 Solvers

Sum of odd numbers in a matrix
554 Solvers

SatCom #8: Satellite Link Budget
29 Solvers
More from this Author17
Problem Tags
Community Treasure Hunt
Find the treasures in MATLAB Central and discover how the community can help you!
Start Hunting!