Hello,
I have project, where I am trying to compute the trajectory of a rocket and also compute when to release a smaller rocket. The code works in general and uses Rungekutta. The main issue is computing the fuelconsumtion/remaining fuel mass. The issue seems that the mass resets after some time and I am not sure the fuel consumtion or fuel mass is computed in the correct manner.
Any help is greatly appriciatedHello,
I have project, where I am trying to compute the trajectory of a rocket and also compute when to release a smaller rocket. The code works in general and uses Rungekutta. The main issue is computing the fuelconsumtion/remaining fuel mass. The issue seems that the mass resets after some time and I am not sure the fuel consumtion or fuel mass is computed in the correct manner.
Any help is greatly appriciated Hello,
I have project, where I am trying to compute the trajectory of a rocket and also compute when to release a smaller rocket. The code works in general and uses Rungekutta. The main issue is computing the fuelconsumtion/remaining fuel mass. The issue seems that the mass resets after some time and I am not sure the fuel consumtion or fuel mass is computed in the correct manner.
Any help is greatly appriciated runge-kutta, rocket trajectory, mass computation, ode MATLAB Answers — New Questions

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