Robust Design of H-infinity Controller for a Launch Vehicle Autopilot against Disturbances

Preprint English OPEN
Graells, Antonio; Carrabina, Francisco;
(2016)

Atmospheric flight phase of a launch vehicle is utilized to evaluate the performance of an H-infinity controller in the presence of disturbances. Dynamics of the vehicle is linearly modeled using time-varying parameters. An operating point was found to design a robust c... View more
Share - Bookmark