Flexible Spacecraft Time-Domain Simulation
This showcases how kdFlex can be used to simulate closed-loop control of a flexible, multibody system. A spacecraft with flexible arms (the links between the spacecraft bus and solar panels) and closed-loop controls changes it's attitude, arm angles, and solar panel angles. Plots in the top-left and top-right show the commanded vs. actual locations of the joints. The spacecraft bus is the Rosetta bus.