My space mission design library allows for pure dynamics, which is best for simulations and mission design, but not state estimation. The goal of this issue is to create an example of using a state transition matrix to compute the linearized dynamics including perturbations.
My space mission design library allows for pure dynamics, which is best for simulations and mission design, but not state estimation. The goal of this issue is to create an example of using a state transition matrix to compute the linearized dynamics including perturbations.