The general equation for the orbital period of a satellite in orbit around the Earth:
T=2*pi*sqrt(a3/muE)
With a equal to the semi-major axis of the orbit (which is the radius r in a circular orbit). The gravitational paramter of the Earth is called muE, and it has the following value...
The AA.BB structure is called spacecraft .model in my own simulation. It will be a 1x1000 structure with the following fields:
[FONT="Courier New"]time
meanJulianDate
position
velocity
I have the following matrices:
[FONT="Courier New"]t [1000x1]
MJD [1000x1]
r [1000x3]
V...
I know the command .*, but don't think it is really what I need. I need to copy the matrix I have into a structure, but it gives errors, which I will post later in this message.
I have this structure AA.BB. This BB has to go from 1 to 1000, which are indications for time steps in a...
Hi,
I have a structure AA.BB, which goes from AA.BB(1) to AA.BB(1000). I have for example a matrix "X" of size [1000x3], which I want to add to this structure, such that it becomes like this:
AA.BB(1).X(1)
AA.BB(2).X(1)
...
AA.BB(1000).X(1)
I want the same for X(2) and X(3).
Can...