The objective of this practice is to calculate the necessary maneuvers to transition from one given initial position and velocity of a satellite to another given final position and velocity by applying external inputs.
First download the code and compile it:
git clone git@github.com:mathUAB/calcul-numeric.git
cd calcul-numeric
chmod +x execute.sh
Then, run the code:
./exectue.sh cmani_rtbp
Type ./exectue.sh for more information about the arguments.