Examples
pos = [6378.e3; 0; 0]; CL_fo_centralAcc(pos) |  |  |
Acceleration due to gravity (central force)
[acc] = CL_fo_centralAcc(pos [, mu])
Acceleration due to the central force (Newtonian acceleration).
It is directed from the central body to the satellite, and is inversely proportional to the distance squared.
Notes:
- The origin for the position vector must be the central body.
- The coordinates frame can be any frame.
See Force models for more details.
Position vector (from the central body) [m]. (3xN)
(optional) Gravitational constant [m^3/s^2]. Default value is %CL_mu. (1x1)
Acceleration [m/s^2]. (3xN)
CNES - DCT/SB
pos = [6378.e3; 0; 0]; CL_fo_centralAcc(pos) | | |