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 Solvers21
Suggested Problems

Project Euler: Problem 2, Sum of even Fibonacci
2163 Solvers

Getting the absolute index from a matrix
242 Solvers

413 Solvers

606 Solvers

325 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!