LMI-based feedback suppression of external disturbances for the RUAV

This paper introduces the stability and controllability augmentation system design for the rotorcraft-based unmanned aerial vehicle. The algorithm of a static output feedback loop shaping for exogenous disturbance suppression of the rotorcraft-based unmanned aerial vehicle in hover is based on the linear matrix inequalities method. Results of the introduced algorithm implementation are evaluated both analytically and with the help of simulation