Vibration control of gyroelastic spacecraft using input shaping and angular momentum devices
Sign Up to like & getrecommendations! Published in 2019 at "Acta Astronautica"
DOI: 10.1016/j.actaastro.2019.03.062
Abstract: Abstract This paper studies the vibration control of gyroelastic spacecraft. The dynamics of gyroelastic spacecraft considering the angular momentum devices are derived using Kane's method. A novel control strategy combining input shaping (IS) and variable-speed… read more here.
Keywords: gyroelastic spacecraft; control; vibration; input shaping ... See more keywords