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Dynamics
bloc0105 edited this page Dec 1, 2024
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Let's use Chrono to perform a real simulation of something. This is a real example coming from my old Engineering classes, so it might be something you'll encounter in the future. What if we wanted to simulate launching a homemade rocket, then letting it fall down back to the ground.
Let's start by setting up our rocket parameters:
- We'll use this rocket. It has a mass of 184g.
- The engine recommended is the D12-5 engine so let's use that.
- For simplicty we'll ignore wind and other factors, we'll also assume the rocket is just going up and down.
#include "chrono/physics/ChSystemNSC.h" // Include Chrono NSC physics system
#include "chrono/physics/ChBody.h" // Include Chrono body
#include <iostream> // Include for console I/O
int main()
{
std::shared_ptr<chrono::ChBody> the_rocket = chrono_types::make_shared<chrono::ChBody>();
the_rocket->SetPos(chrono::ChVector3d(0.0, 0.0, 0.0));
the_rocket->SetMass(0.184);
chrono::ChVector3d impulse_force(0, 30, 0);
chrono::ChVector3d steady_force(0, 10, 0);
double impulse_time = 0.3;
double steady_time = 1.6;
chrono::ChSystemNSC physics_system = chrono::ChSystemNSC();
physics_system.Add(the_rocket);
double timestep = 0.01;
size_t time_counter = 0;
while (the_rocket->GetPos()[1] >= 0 || time_counter == 0)
{
double sim_time = (double)time_counter * timestep;
if (sim_time < impulse_time)
{
the_rocket->AccumulateForce(impulse_force, the_rocket->GetPos(), false);
}
else if (sim_time < steady_time)
{
the_rocket->AccumulateForce(steady_force, the_rocket->GetPos(), false);
}
physics_system.DoStepDynamics(timestep);
the_rocket->EmptyAccumulators();
time_counter++;
std::cout << sim_time << ", " << the_rocket->GetPos()[1] << std::endl;
}
stream_out.close();
return 0;
}
Let's break down exactly what the simulation does:
- There is an initial force of 30N for .3 seconds
- After that, the engine gives off a force of 10N for up to 1.6 seconds.
- The rocket then follows a parabolic trajectory according to gravity. We use Chrono's default gravity of 1g (9.81m/s^2^) in the y-direction.
- The simulation stops when the rocket reaches the ground.
The final output can be plotted as a function of time:
- Real Rockets deploy a parachute after a delay time. Lookup the delay time and see how to add this into your simulation. Asume a constant fall-rate after the parachute is deployed.
- In order to get the plot, I had to use a filestream output instead of just
std::cout
. See if you can get Chrono to save to a file.