Asymptotically decoupled discontinuous control of systems and nonlinear aircraft maneuver
作者： S.N. Singh
DOI: 10.1109/7.30793
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摘要: The question of control a class nonlinear systems that can be decoupled by state-variable feedback is considered. Based on variable-structure system theory, discontinuous law derived accomplishes asymptotic output trajectory-following in the presence uncertainty system. In closed-loop system, trajectories are attracted toward chosen hypersurface state space and then slide along it. During sliding phase motion insensitive to parameter variations. this result, for asymptotically roll angle, angle attack, sideslip rapid, maneuvers derived. Simulation results presented show large, simultaneous lateral longitudinal performed spite stability derivatives. >
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