The question of control of a class of nonlinear systems that can be decoupled by state-variable feedback is considered. Based on variable-structure system theory, a discontinuous control law is derived that accomplishes asymptotic decoupled output trajectory-following in the presence of uncertainty in the system. In the closed-loop system, the trajectories are attracted toward a chosen hypersurface in the state space and then slide along it. During the sliding phase the motion is insensitive to parameter variations. Based on this result, a control law for asymptotically decoupled control of roll angle, angle of attack, and sideslip in rapid, nonlinear maneuvers is derived. Simulation results are presented to show that large, simultaneous lateral and longitudinal maneuvers can be performed in spite of uncertainty in the stability derivatives.<>
Asymptotically decoupled discontinuous control of systems and nonlinear aircraft maneuver
IEEE Transactions on Aerospace and Electronic Systems ; 25 , 3 ; 380-391
01.05.1989
717797 byte
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Decoupled ultimate boundedness control of systems and large aircraft maneuver
Tema Archiv | 1989
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