Robust Design of H∞Controller for a Launch Vehicle Autopilot against Disturbances
نویسندگان
چکیده
منابع مشابه
Robust Design of H-infinity Controller for a Launch Vehicle Autopilot against Disturbances
Atmospheric flight phase of a launch vehicle is utilized to evaluate the performance of an H∞ 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 command tracker using H∞ control theory that guarantees a stable maneuver. At the end, the controller was employed on the launch vehicle...
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ژورنال
عنوان ژورنال: IOSR Journal of Electrical and Electronics Engineering
سال: 2016
ISSN: 2320-3331,2278-1676
DOI: 10.9790/1676-110502135140