/Rocket-Attitude-Dynamics

Attitude control of a rocket in atmosferic flight

Primary LanguageMATLABGNU General Public License v3.0GPL-3.0

Attitude control of a rocket in atmosferic flight

Authors: Domenico Trotta, Alessandro Zavoli, Guido De Matteis

Numerical data

  • GreensiteLPV_DATA.txt: LV model parameters
  • Controller.txt: PD controller gain and LP filter data

MATLAB/Simulink LV Model

  • Sim_Init.m : Load in MATLAB WorkSpace LV data for LV_Greensite.slx, that are:
    • GreensiteLPV_DATA.mat: timeseries of LV parameters
    • Controller.mat: PD controller gain and LP filter data
    • Drywind.mat: High altitude Dryden wind model parameters
    • Qmax.mat: Aerodynamics load safty envelope data
    • gain_delay_state_model.m: function to create delay padè approximantion transfer function
  • LV_Greensite.slx: Simulink model including launch vehicle and wind models. baseline controller active