摘要：AbstractIn this paper, a step-by-step procedure to design a robust H∞controller for the attitude control of a launch vehicle has been proposed. A model of a typical launch vehicle has been considered to carry out the study. Later on, the performance of the system with H∞controller has been compared with that of a classical controller. The H∞optimization is efficient as well as an effective approach for the design of a robust controller. Along with the required performance, the H∞controller ensures the robustness of the system against uncertainties, noises, and disturbances.
关键词：KeywordsLaunch VehicleH-infinity controllerRobust ControlAttitude Control
